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Nose cone design

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82: 3205: 1658: 2938: 2582: 1649: 395: 2005: 2917: 2601: 2563: 25: 386: 3640: 3226: 1415: 1973: 3659: 2448: 758: 1406: 3190: 2902: 214: 2439: 3690: 205: 749: 3581: 3734:, particularly at low ratios; but there is very little additional gain for ratios increasing beyond 5:1. As the fineness ratio increases, the wetted area, and thus the skin friction component of drag, will also increase. Therefore, the minimum drag fineness ratio will ultimately be a trade-off between the decreasing wave drag and increasing friction drag. 1928: 3495: 1996: 1964: 2969:
is a member of the parabolic series (described above). The power series shape is characterized by its (usually) blunt tip, and by the fact that its base is not tangent to the body tube. There is always a discontinuity at the joint between nose cone and body that looks distinctly non-aerodynamic. The
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This observation goes against the often-repeated conventional wisdom that a conical nose is optimum for "Mach-breaking". Fighter aircraft are probably good examples of nose shapes optimized for the transonic region, although their nose shapes are often distorted by other considerations of avionics
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Many references on nose cone design contain empirical data comparing the drag characteristics of various nose shapes in different flight regimes. The chart shown here seems to be the most comprehensive and useful compilation of data for the flight regime of greatest interest. This chart generally
2633:. This construction is similar to that of the tangent ogive, except that a parabola is the defining shape rather than a circle. Just as it does on an ogive, this construction produces a nose shape with a sharp tip. For the blunt shape typically associated with a parabolic nose, see 1682: 3311: 2207: 2788: 232:. This shape is often chosen for its ease of manufacture. More optimal, streamlined shapes (described below) are often much more difficult to create. The sides of a conic profile are straight lines, so the diameter equation is simply: 2331: 2344:
and greater than half the length of the nose cone, then the result will be a secant ogive that bulges out to a maximum diameter that is greater than the base diameter. A classic example of this shape is the nose cone of the
511: 2035:(as it is for a tangent ogive), but rather is one of the factors to be chosen to define the nose shape. If the chosen ogive radius of a secant ogive is greater than the ogive radius of a tangent ogive with the same 1309: 3626:
region and beyond, where the pressure drag increases dramatically, the effect of nose shape on drag becomes highly significant. The factors influencing the pressure drag are the general shape of the nose cone, its
3723:, though that term is usually applied to wings and tails. Fineness ratio is often applied to the entire vehicle, considering the overall length and diameter. The length/diameter relation is also often called the 1923:{\displaystyle {\begin{aligned}x_{o}&=L-{\sqrt {\left(\rho -r_{n}\right)^{2}-(\rho -R)^{2}}}\\y_{t}&={\frac {r_{n}(\rho -R)}{\rho -r_{n}}}\\x_{t}&=x_{o}-{\sqrt {r_{n}^{2}-y_{t}^{2}}}\end{aligned}}} 1445:
to the curve of the nose cone at its base, and the base is on the radius of the circle. The popularity of this shape is largely due to the ease of constructing its profile, as it is simply a circular section.
1176: 2423: 3490:{\displaystyle {\begin{aligned}\theta (x)&=\arccos \left(1-{2x \over L}\right)\\y(\theta ,C)&={R \over {\sqrt {\pi }}}{\sqrt {\theta -{\sin(2\theta ) \over 2}+C\sin ^{3}(\theta )}}\end{aligned}}} 1100: 2889:
result in a slimmer shape, whose appearance is similar to that of the secant ogive. The shape is no longer tangent at the base, and the base is parallel to, but offset from, the axis of the parabola.
667: 3622:, the surface smoothness of that area, and the presence of any discontinuities in the shape. For example, in strictly subsonic rockets a short, blunt, smooth elliptical shape is usually best. In the 1618: 2474:) due to the blunt nose and tangent base. This is not a shape normally found in professional rocketry, which almost always flies at much higher velocities where other designs are more suitable. If 328: 3316: 1687: 2547: 1390: 3113: 2104: 1518: 2625:
This nose shape is not the blunt shape that is envisioned when people commonly refer to a "parabolic" nose cone. The parabolic series nose shape is generated by rotating a segment of a
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The profile of this shape is also formed by a segment of a circle, but the base of the shape is not on the radius of the circle defined by the ogive radius. The rocket body will
997: 904: 733: 370: 271: 3062: 863: 2680: 191:. While the equations describe the "perfect" shape, practical nose cones are often blunted or truncated for manufacturing, aerodynamic, or thermodynamic reasons. 3291:
indicates minimum drag for a given length and volume. The Haack series nose cones are not perfectly tangent to the body at their base except for the case where
2466:, with the major axis being the centerline and the minor axis being the base of the nose cone. A rotation of a full ellipse about its major axis is called a 2238: 3757: 3305:, Haack nose cones bulge to a maximum diameter greater than the base diameter. Haack nose tips do not come to a sharp point, but are slightly rounded. 423: 3618:.8, the nose pressure drag is essentially zero for all shapes. The major significant factor is friction drag, which is largely dependent upon the 3812: 1231: 2470:
spheroid, so an elliptical nose shape would properly be known as a prolate hemispheroid. This shape is popular in subsonic flight (such as
3253:'s series shapes are not constructed from geometric figures. The shapes are instead mathematically derived for the purpose of minimizing 1113: 2355: 1002: 592: 3702: 1549: 286: 3678:
1.2. Although data are not available for many shapes in the transonic region, the table clearly suggests that either the
2492: 1314: 3067: 2049: 68: 46: 39: 3879: 2202:{\displaystyle \alpha =\arccos \left({{\sqrt {L^{2}+R^{2}}} \over 2\rho }\right)-\arctan \left({R \over L}\right)} 1463: 3789: 3602:
An aerospike can be used to reduce the forebody pressure acting on supersonic aircraft. The aerospike creates a
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geometrical shape for optimum performance. For many applications, such a task requires the definition of a
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In many nose cone designs, the greatest concern is flight performance in the transonic region from Mach
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includes the shape commonly referred to as a "parabolic" nose cone, but the shape correctly known as a
963: 870: 685: 333: 3779: 2783:{\displaystyle y=R\left({2\left({x \over L}\right)-K'\left({x \over L}\right)^{2} \over 2-K'}\right)} 1657: 2643: 238: 3819: 3651:
agrees with more detailed, but less comprehensive data found in other references (most notably the
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The Haack series designs giving minimum drag for the given length and diameter, the LD-Haack where
3035: 2043:, then the resulting secant ogive appears as a tangent ogive with a portion of the base truncated. 822: 33: 3597: 2937: 1457:, and it is related to the length and base radius of the nose cone as expressed by the formula: 50: 3917: 3693: 2581: 1648: 394: 3258: 8: 3845: 2971: 129: 2004: 3860: 2916: 174: 132:
shape that experiences minimal resistance to rapid motion through such a fluid medium.
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shape can be modified at the base to smooth out this discontinuity. Both a flat-faced
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Geometry and construction of the foremost tip of airplanes, spacecraft and projectiles
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The ratio of the length of a nose cone compared to its base diameter is known as the
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Alternate secant ogive render and profile which show a bulge due to a smaller radius.
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Spherically blunted tangent ogive nose cone render and profile with parameters shown.
2600: 2562: 385: 3585: 3225: 2326:{\displaystyle y={\sqrt {\rho ^{2}-(\rho \cos(\alpha )-x)^{2}}}-\rho \sin(\alpha )} 410: 3666:
to low-mach regions. Rankings are: superior (1), good (2), fair (3), inferior (4).
1676:. The tangency point where the sphere meets the tangent ogive can be found from: 1423:
Tangent ogive nose cone render and profile with parameters and ogive circle shown.
3679: 2975: 1414: 229: 3686:, would be preferable to the popular conical or ogive shapes, for this purpose. 3028:
decreases towards zero, the power series nose shape becomes increasingly blunt.
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to the body at its base, and the base is on the axis of the parabola. Values of
1972: 506:{\displaystyle x_{t}={\frac {L^{2}}{R}}{\sqrt {\frac {r_{n}^{2}}{R^{2}+L^{2}}}}} 3730:
At supersonic speeds, the fineness ratio has a significant effect on nose cone
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below. (The parabolic shape is also often confused with the elliptical shape.)
2471: 1434: 173:. The equations define the two-dimensional profile of the nose shape. The full 81: 3298:. However, the discontinuity is usually so slight as to be imperceptible. For 2447: 3911: 3897: 403:
Spherically blunted conic nose cone render and profile with parameters shown.
3658: 3261:. While the series is a continuous set of shapes determined by the value of 757: 2630: 1995: 1963: 1984:
ogive nose cone render and profile with parameters and ogive circle shown.
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of the nose cone is formed by rotating the profile around the centerline
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A tangent ogive nose is often blunted by capping it with a segment of a
1304:{\displaystyle \phi _{2}=\arctan \left({R_{2}-R_{1} \over L_{2}}\right)} 417:. The tangency point where the sphere meets the cone can be found from: 3644: 2438: 3662:
Comparison of drag characteristics of various nose cone shapes in the
3731: 3663: 3623: 748: 125: 97: 413:, a conical nose is often blunted by capping it with a segment of a 204: 3580: 3280:
signifies minimum drag for the given length and diameter, and when
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ahead of the body, thus reducing the drag acting on the aircraft.
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be tangent to the curve of the nose at its base. The ogive radius
1171:{\displaystyle \phi _{1}=\arctan \left({R_{1} \over L_{1}}\right)} 3689: 2875: 2467: 2463: 2418:{\displaystyle {\frac {L}{2}}<\rho <{R^{2}+L^{2} \over 2R}} 1442: 782: 113: 3889: 2483: 1673: 1632: 1438: 414: 121: 105: 93: 3765:
Bericht 139 der Lilienthal-Gesellschaft für Luftfahrtforschung
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Elliptical nose cone render and profile with parameters shown.
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nose appears to be a very close match to a Von Kármán shape.
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International Research Journal of Engineering and Technology
3846:"A Review on Nose Cone Designs for Different Flight Regimes" 2806:, but the most common values used for nose cone shapes are: 1449:
The radius of the circle that forms the ogive is called the
1095:{\displaystyle y=R_{1}+{(x-L_{1})(R_{2}-R_{1}) \over L_{2}}} 766:
Bi-conic nose cone render and profile with parameters shown.
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General parameters used for constructing nose cone profiles.
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to the top radius of the smaller frustum with base radius
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The power series nose shape is generated by rotating the
662:{\displaystyle x_{o}=x_{t}+{\sqrt {r_{n}^{2}-y_{t}^{2}}}} 222:
Conic nose cone render and profile with parameters shown.
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section of any vehicle or body meant to travel through a
1437:. The profile of this shape is formed by a segment of a 772:
A bi-conic nose cone shape is simply a cone with length
1613:{\displaystyle y={\sqrt {\rho ^{2}-(L-x)^{2}}}+R-\rho } 798:, where the base of the upper cone is equal in radius 323:{\displaystyle \phi =\arctan \left({R \over L}\right)} 3314: 3070: 3038: 2683: 2646: 2495: 2358: 2241: 2112: 2052: 1685: 1552: 1466: 1317: 1234: 1184: 1116: 1005: 966: 912: 873: 825: 688: 595: 520: 426: 336: 289: 241: 3257:; a related shape with similar derivation being the 1638: 124:), an important problem is the determination of the 3696:
with a nose cone very close to the Von Kármán shape
3016:controls the bluntness of the shape. For values of 145:In all of the following nose cone shape equations, 3708: 3489: 3107: 3056: 2782: 2669: 2542:{\displaystyle y=R{\sqrt {1-{x^{2} \over L^{2}}}}} 2541: 2417: 2325: 2201: 2098: 1922: 1612: 1512: 1385:{\displaystyle y=R_{1}+(x-L_{1})\tan(\phi _{2})\;} 1384: 1303: 1219: 1170: 1094: 991: 950: 898: 857: 727: 661: 558: 505: 364: 322: 265: 3785:Design of Aerodynamically Stabilized Free Rockets 3634: 3609: 3193:Graphs illustrating Haack series nose cone shapes 2905:Graphs illustrating power series nose cone shapes 276:Cones are sometimes defined by their half angle, 135: 3909: 3844:Iyer, Aditya Rajan; Pant, Anjali (August 2020). 3108:{\displaystyle y=R\left({x \over L}\right)^{n}} 2099:{\displaystyle \rho >{R^{2}+L^{2} \over 2R}} 2619:Renders of common parabolic nose cone shapes. 3758:"Geschoßformen kleinsten Wellenwiderstandes" 2462:The profile of this shape is one-half of an 1513:{\displaystyle \rho ={R^{2}+L^{2} \over 2R}} 375: 153:is the radius of the base of the nose cone. 3810: 149:is the overall length of the nose cone and 3249:Unlike all of the nose cone shapes above, 1381: 1216: 361: 228:A very common nose-cone shape is a simple 1947:is the center of the spherical nose cap. 1631:. If they are equal, then the shape is a 576:is the radius of the spherical nose cap. 559:{\displaystyle y_{t}={\frac {x_{t}R}{L}}} 69:Learn how and when to remove this message 3843: 3688: 3657: 3638: 3579: 3188: 2900: 80: 32:This article includes a list of general 3910: 3813:The Descriptive Geometry of Nose Cones 3804: 3265:in the equations below, two values of 951:{\displaystyle y={xR_{1} \over L_{1}}} 579:The center of the spherical nose cap, 3755: 140: 3877: 3871: 3837: 3719:. This is sometimes also called the 1220:{\displaystyle y=x\tan(\phi _{1})\;} 18: 3269:have particular significance: when 2867:For the case of the full parabola ( 1429:Next to a simple cone, the tangent 13: 3749: 3682:shape, or power series shape with 409:In practical applications such as 169:, at the tip of the nose cone, to 38:it lacks sufficient corresponding 14: 3934: 3643:Closeup view of a nose cone on a 2978:are members of the power series. 2634: 1639:Spherically blunted tangent ogive 992:{\displaystyle L_{1}\leq x\leq L} 899:{\displaystyle 0\leq x\leq L_{1}} 728:{\displaystyle x_{a}=x_{o}-r_{n}} 3614:For aircraft and rockets, below 3224: 3203: 2936: 2915: 2599: 2580: 2561: 2446: 2437: 2003: 1994: 1971: 1962: 1656: 1647: 1627:, must be less than or equal to 1413: 1404: 1395: 756: 747: 393: 384: 365:{\displaystyle y=x\tan(\phi )\;} 212: 203: 23: 3790:U.S. Government Printing Office 3709:Influence of the fineness ratio 3180: 2892: 2340:is less than the tangent ogive 1953: 785:of a cone (commonly known as a 3884:. New York City: McGraw-Hill. 3635:Influence of the general shape 3610:Nose cone drag characteristics 3504:(as described above) include: 3478: 3472: 3444: 3435: 3394: 3382: 3328: 3322: 3024:, the tip is fairly sharp. As 2670:{\displaystyle 0\leq K'\leq 1} 2629:around a line parallel to its 2320: 2314: 2291: 2281: 2275: 2263: 1821: 1809: 1764: 1751: 1587: 1574: 1433:shape is the most familiar in 1378: 1365: 1356: 1337: 1213: 1200: 1076: 1050: 1047: 1028: 358: 352: 266:{\displaystyle y={xR \over L}} 136:Nose cone shapes and equations 1: 3811:Crowell Sr., Gary A. (1996). 3797: 3552: 3057:{\displaystyle 0\leq n\leq 1} 2428: 1441:such that the rocket body is 858:{\displaystyle L=L_{1}+L_{2}} 3881:Missile Configuration Design 3701:and inlets. For example, an 3591: 2552: 7: 3737: 3631:, and its bluffness ratio. 738: 157:is the radius at any point 10: 3939: 3744:Index of aviation articles 3595: 2798:can vary anywhere between 787:conical transition section 3780:U.S. Army Missile Command 3564:, is commonly called the 376:Spherically blunted conic 89:Given the problem of the 3818:(Report). Archived from 3756:Haack, Wolfgang (1941). 194: 3767:: 14–28. Archived from 3598:Drag-reducing aerospike 3210:LD-Haack (Von Kármán) ( 53:more precise citations. 3697: 3667: 3647: 3588: 3521:LD-Haack (Von Kármán) 3491: 3194: 3109: 3058: 2906: 2784: 2671: 2543: 2419: 2327: 2203: 2100: 1924: 1623:The nose cone length, 1614: 1514: 1386: 1305: 1221: 1172: 1096: 993: 952: 900: 859: 729: 663: 560: 507: 366: 324: 267: 86: 3694:General Dynamics F-16 3692: 3661: 3642: 3583: 3492: 3192: 3110: 3059: 2904: 2785: 2672: 2544: 2420: 2328: 2204: 2101: 2027:is not determined by 1925: 1615: 1515: 1387: 1306: 1222: 1173: 1097: 994: 953: 901: 860: 730: 664: 586:, can be found from: 561: 508: 367: 325: 268: 84: 3878:Chin, S. S. (1961). 3703:F-16 Fighting Falcon 3584:An aerospike on the 3312: 3068: 3036: 3004:-axis for values of 2681: 2644: 2493: 2356: 2239: 2110: 2050: 1683: 1550: 1464: 1315: 1232: 1182: 1114: 1003: 964: 910: 871: 823: 781:stacked on top of a 686: 672:And the apex point, 593: 518: 424: 334: 287: 239: 3792:. MIL-HDBK-762(MI). 2967:parabolic nose cone 1913: 1895: 789:shape) with length 679:can be found from: 656: 638: 474: 130:solid of revolution 3698: 3668: 3648: 3589: 3510:Haack series type 3500:Special values of 3487: 3485: 3195: 3105: 3054: 2907: 2780: 2667: 2539: 2415: 2323: 2199: 2096: 1940:is the radius and 1920: 1918: 1899: 1881: 1610: 1510: 1382: 1301: 1217: 1168: 1092: 989: 948: 896: 855: 725: 659: 642: 624: 556: 503: 460: 362: 320: 263: 175:body of revolution 141:General dimensions 104:medium (such as a 102:compressible fluid 87: 3550: 3549: 3481: 3451: 3416: 3414: 3368: 3247: 3246: 3178: 3177: 3118:Common values of 3093: 2959: 2958: 2865: 2864: 2774: 2745: 2715: 2537: 2535: 2413: 2367: 2300: 2193: 2166: 2156: 2094: 1914: 1843: 1773: 1596: 1508: 1295: 1162: 1090: 946: 657: 554: 501: 500: 455: 411:re-entry vehicles 314: 261: 79: 78: 71: 3930: 3902: 3901: 3875: 3869: 3868: 3859:(8): 3546–3554. 3850: 3841: 3835: 3834: 3832: 3830: 3825:on 11 April 2011 3824: 3817: 3808: 3793: 3782:(17 July 1990). 3775: 3773: 3762: 3727:of a nose cone. 3685: 3677: 3673: 3586:UGM-96 Trident I 3563: 3546: 3536: 3526: 3515: 3507: 3506: 3503: 3496: 3494: 3493: 3488: 3486: 3482: 3468: 3467: 3452: 3447: 3427: 3419: 3417: 3415: 3410: 3405: 3374: 3370: 3369: 3364: 3356: 3304: 3297: 3290: 3286: 3279: 3275: 3268: 3264: 3259:Sears–Haack body 3237: 3228: 3216: 3207: 3185: 3184: 3174: 3164: 3154: 3149:Half (parabola) 3144: 3133: 3125: 3124: 3121: 3114: 3112: 3111: 3106: 3104: 3103: 3098: 3094: 3086: 3063: 3061: 3060: 3055: 3027: 3023: 3019: 3015: 3011: 3007: 3003: 3000:curve about the 2999: 2949: 2940: 2928: 2919: 2897: 2896: 2888: 2884: 2873: 2861: 2851: 2841: 2831: 2820: 2809: 2808: 2805: 2801: 2797: 2789: 2787: 2786: 2781: 2779: 2775: 2773: 2772: 2757: 2756: 2755: 2750: 2746: 2738: 2731: 2720: 2716: 2708: 2698: 2676: 2674: 2673: 2668: 2660: 2612: 2603: 2593: 2584: 2574: 2565: 2548: 2546: 2545: 2540: 2538: 2536: 2534: 2533: 2524: 2523: 2514: 2506: 2481: 2477: 2450: 2441: 2424: 2422: 2421: 2416: 2414: 2412: 2404: 2403: 2402: 2390: 2389: 2379: 2368: 2360: 2343: 2339: 2332: 2330: 2329: 2324: 2301: 2299: 2298: 2259: 2258: 2249: 2231: 2227: 2223: 2219: 2215: 2212:Then the radius 2208: 2206: 2205: 2200: 2198: 2194: 2186: 2171: 2167: 2165: 2157: 2155: 2154: 2142: 2141: 2132: 2130: 2105: 2103: 2102: 2097: 2095: 2093: 2085: 2084: 2083: 2071: 2070: 2060: 2042: 2038: 2034: 2030: 2026: 2007: 1998: 1975: 1966: 1946: 1939: 1929: 1927: 1926: 1921: 1919: 1915: 1912: 1907: 1894: 1889: 1880: 1875: 1874: 1858: 1857: 1844: 1842: 1841: 1840: 1824: 1808: 1807: 1797: 1788: 1787: 1774: 1772: 1771: 1747: 1746: 1741: 1737: 1736: 1735: 1714: 1699: 1698: 1660: 1651: 1630: 1626: 1619: 1617: 1616: 1611: 1597: 1595: 1594: 1570: 1569: 1560: 1542: 1538: 1534: 1530: 1526: 1519: 1517: 1516: 1511: 1509: 1507: 1499: 1498: 1497: 1485: 1484: 1474: 1456: 1417: 1408: 1391: 1389: 1388: 1383: 1377: 1376: 1355: 1354: 1333: 1332: 1310: 1308: 1307: 1302: 1300: 1296: 1294: 1293: 1284: 1283: 1282: 1270: 1269: 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3927: 3908: 3907: 3906: 3905: 3876: 3872: 3848: 3842: 3838: 3828: 3826: 3822: 3815: 3809: 3805: 3800: 3771: 3760: 3752: 3750:Further reading 3740: 3711: 3683: 3675: 3671: 3637: 3612: 3600: 3594: 3558: 3555: 3544: 3534: 3524: 3513: 3501: 3484: 3483: 3463: 3459: 3428: 3426: 3418: 3409: 3404: 3397: 3376: 3375: 3357: 3355: 3348: 3344: 3331: 3315: 3313: 3310: 3309: 3299: 3292: 3288: 3281: 3277: 3276:, the notation 3270: 3266: 3262: 3243: 3242: 3241: 3240: 3239: 3232: 3229: 3220: 3219: 3218: 3211: 3208: 3183: 3172: 3162: 3152: 3142: 3131: 3119: 3099: 3085: 3081: 3080: 3069: 3066: 3065: 3037: 3034: 3033: 3025: 3021: 3017: 3013: 3009: 3005: 3001: 2982: 2955: 2954: 2953: 2952: 2951: 2944: 2943:Three-quarter ( 2941: 2932: 2931: 2930: 2923: 2920: 2895: 2886: 2879: 2874:) the shape is 2868: 2859: 2849: 2839: 2829: 2815: 2803: 2799: 2792: 2765: 2758: 2751: 2737: 2733: 2732: 2724: 2707: 2703: 2699: 2697: 2693: 2682: 2679: 2678: 2653: 2645: 2642: 2641: 2623: 2622: 2621: 2620: 2616: 2615: 2614: 2607: 2604: 2596: 2595: 2588: 2587:Three-quarter ( 2585: 2577: 2576: 2569: 2566: 2555: 2529: 2525: 2519: 2515: 2513: 2505: 2494: 2491: 2490: 2479: 2475: 2460: 2459: 2458: 2457: 2453: 2452: 2451: 2443: 2442: 2431: 2405: 2398: 2394: 2385: 2381: 2380: 2378: 2359: 2357: 2354: 2353: 2341: 2337: 2294: 2290: 2254: 2250: 2248: 2240: 2237: 2236: 2229: 2225: 2221: 2217: 2213: 2185: 2181: 2158: 2150: 2146: 2137: 2133: 2131: 2129: 2125: 2111: 2108: 2107: 2086: 2079: 2075: 2066: 2062: 2061: 2059: 2051: 2048: 2047: 2040: 2036: 2032: 2028: 2024: 2017: 2016: 2015: 2014: 2010: 2009: 2008: 2000: 1999: 1988: 1987: 1986: 1985: 1978: 1977: 1976: 1968: 1967: 1956: 1950: 1945: 1941: 1938: 1934: 1917: 1916: 1908: 1903: 1890: 1885: 1879: 1870: 1866: 1859: 1853: 1849: 1846: 1845: 1836: 1832: 1825: 1803: 1799: 1798: 1796: 1789: 1783: 1779: 1776: 1775: 1767: 1763: 1742: 1731: 1727: 1720: 1716: 1715: 1713: 1700: 1694: 1690: 1686: 1684: 1681: 1680: 1670: 1669: 1668: 1667: 1663: 1662: 1661: 1653: 1652: 1641: 1628: 1624: 1590: 1586: 1565: 1561: 1559: 1551: 1548: 1547: 1540: 1536: 1532: 1528: 1524: 1500: 1493: 1489: 1480: 1476: 1475: 1473: 1465: 1462: 1461: 1454: 1427: 1426: 1425: 1424: 1420: 1419: 1418: 1410: 1409: 1398: 1372: 1368: 1350: 1346: 1328: 1324: 1316: 1313: 1312: 1289: 1285: 1278: 1274: 1265: 1261: 1260: 1258: 1254: 1239: 1235: 1233: 1230: 1229: 1207: 1203: 1183: 1180: 1179: 1156: 1152: 1146: 1142: 1140: 1136: 1121: 1117: 1115: 1112: 1111: 1084: 1080: 1070: 1066: 1057: 1053: 1041: 1037: 1027: 1025: 1016: 1012: 1004: 1001: 1000: 971: 967: 965: 962: 961: 940: 936: 929: 925: 921: 919: 911: 908: 907: 890: 886: 872: 869: 868: 849: 845: 836: 832: 824: 821: 820: 814: 808: 805: 799: 796: 790: 779: 773: 770: 769: 768: 767: 763: 762: 761: 753: 752: 741: 719: 715: 706: 702: 693: 689: 687: 684: 683: 677: 673: 651: 646: 633: 628: 622: 613: 609: 600: 596: 594: 591: 590: 584: 580: 574: 570: 541: 537: 536: 534: 525: 521: 519: 516: 515: 493: 489: 480: 476: 475: 469: 464: 457: 446: 442: 440: 431: 427: 425: 422: 421: 407: 406: 405: 404: 400: 399: 398: 390: 389: 378: 335: 332: 331: 306: 302: 288: 285: 284: 277: 250: 248: 240: 237: 236: 226: 225: 224: 223: 219: 218: 217: 209: 208: 197: 186: 185: 180: 179: 178: 170: 166: 162: 158: 154: 150: 146: 143: 138: 75: 64: 58: 55: 45:Please help to 44: 28: 24: 17: 12: 11: 5: 3936: 3926: 3925: 3920: 3904: 3903: 3870: 3836: 3802: 3801: 3799: 3796: 3795: 3794: 3776: 3774:on 2007-09-27. 3751: 3748: 3747: 3746: 3739: 3736: 3716:fineness ratio 3710: 3707: 3636: 3633: 3629:fineness ratio 3611: 3608: 3604:detached shock 3596:Main article: 3593: 3590: 3554: 3551: 3548: 3547: 3542: 3538: 3537: 3532: 3528: 3527: 3522: 3518: 3517: 3511: 3498: 3497: 3480: 3477: 3474: 3471: 3466: 3462: 3458: 3455: 3450: 3446: 3443: 3440: 3437: 3434: 3431: 3425: 3422: 3413: 3408: 3403: 3400: 3398: 3396: 3393: 3390: 3387: 3384: 3381: 3378: 3377: 3373: 3367: 3363: 3360: 3354: 3351: 3347: 3343: 3340: 3337: 3334: 3332: 3330: 3327: 3324: 3321: 3318: 3317: 3251:Wolfgang Haack 3245: 3244: 3230: 3223: 3222: 3221: 3209: 3202: 3201: 3200: 3199: 3198: 3196: 3182: 3179: 3176: 3175: 3170: 3166: 3165: 3160: 3159:Three quarter 3156: 3155: 3150: 3146: 3145: 3140: 3136: 3135: 3129: 3116: 3115: 3102: 3097: 3092: 3089: 3084: 3079: 3076: 3073: 3053: 3050: 3047: 3044: 3041: 2957: 2956: 2942: 2935: 2934: 2933: 2921: 2914: 2913: 2912: 2911: 2910: 2908: 2894: 2891: 2863: 2862: 2857: 2853: 2852: 2847: 2846:Three quarter 2843: 2842: 2837: 2833: 2832: 2827: 2823: 2822: 2813: 2812:Parabola type 2778: 2771: 2768: 2764: 2761: 2754: 2749: 2744: 2741: 2736: 2730: 2727: 2723: 2719: 2714: 2711: 2706: 2702: 2696: 2692: 2689: 2686: 2666: 2663: 2659: 2656: 2652: 2649: 2618: 2617: 2605: 2598: 2597: 2586: 2579: 2578: 2567: 2560: 2559: 2558: 2557: 2556: 2554: 2551: 2550: 2549: 2532: 2528: 2522: 2518: 2512: 2509: 2504: 2501: 2498: 2472:model rocketry 2455: 2454: 2445: 2444: 2436: 2435: 2434: 2433: 2432: 2430: 2427: 2426: 2425: 2411: 2408: 2401: 2397: 2393: 2388: 2384: 2377: 2374: 2371: 2366: 2363: 2336:If the chosen 2334: 2333: 2322: 2319: 2316: 2313: 2310: 2307: 2304: 2297: 2293: 2289: 2286: 2283: 2280: 2277: 2274: 2271: 2268: 2265: 2262: 2257: 2253: 2247: 2244: 2210: 2209: 2197: 2192: 2189: 2184: 2180: 2177: 2174: 2170: 2164: 2161: 2153: 2149: 2145: 2140: 2136: 2128: 2124: 2121: 2118: 2115: 2092: 2089: 2082: 2078: 2074: 2069: 2065: 2058: 2055: 2012: 2011: 2002: 2001: 1993: 1992: 1991: 1990: 1989: 1980: 1979: 1970: 1969: 1961: 1960: 1959: 1958: 1957: 1955: 1952: 1943: 1936: 1931: 1930: 1911: 1906: 1902: 1898: 1893: 1888: 1884: 1878: 1873: 1869: 1865: 1862: 1860: 1856: 1852: 1848: 1847: 1839: 1835: 1831: 1828: 1823: 1820: 1817: 1814: 1811: 1806: 1802: 1795: 1792: 1790: 1786: 1782: 1778: 1777: 1770: 1766: 1762: 1759: 1756: 1753: 1750: 1745: 1740: 1734: 1730: 1726: 1723: 1719: 1712: 1709: 1706: 1703: 1701: 1697: 1693: 1689: 1688: 1665: 1664: 1655: 1654: 1646: 1645: 1644: 1643: 1642: 1640: 1637: 1621: 1620: 1609: 1606: 1603: 1600: 1593: 1589: 1585: 1582: 1579: 1576: 1573: 1568: 1564: 1558: 1555: 1521: 1520: 1506: 1503: 1496: 1492: 1488: 1483: 1479: 1472: 1469: 1435:hobby rocketry 1422: 1421: 1412: 1411: 1403: 1402: 1401: 1400: 1399: 1397: 1394: 1393: 1392: 1380: 1375: 1371: 1367: 1364: 1361: 1358: 1353: 1349: 1345: 1342: 1339: 1336: 1331: 1327: 1323: 1320: 1299: 1292: 1288: 1281: 1277: 1273: 1268: 1264: 1257: 1253: 1250: 1247: 1242: 1238: 1227: 1215: 1210: 1206: 1202: 1199: 1196: 1193: 1190: 1187: 1166: 1159: 1155: 1149: 1145: 1139: 1135: 1132: 1129: 1124: 1120: 1103: 1102: 1087: 1083: 1078: 1073: 1069: 1065: 1060: 1056: 1052: 1049: 1044: 1040: 1036: 1033: 1030: 1024: 1019: 1015: 1011: 1008: 988: 985: 982: 979: 974: 970: 958: 943: 939: 932: 928: 924: 918: 915: 893: 889: 885: 882: 879: 876: 865: 852: 848: 844: 839: 835: 831: 828: 812: 803: 794: 777: 765: 764: 755: 754: 746: 745: 744: 743: 742: 740: 737: 736: 735: 722: 718: 714: 709: 705: 701: 696: 692: 675: 670: 669: 654: 649: 645: 641: 636: 631: 627: 621: 616: 612: 608: 603: 599: 582: 572: 567: 566: 553: 549: 544: 540: 533: 528: 524: 513: 496: 492: 488: 483: 479: 472: 467: 463: 454: 449: 445: 439: 434: 430: 402: 401: 392: 391: 383: 382: 381: 380: 379: 377: 374: 373: 372: 360: 357: 354: 351: 348: 345: 342: 339: 318: 313: 310: 305: 301: 298: 295: 292: 274: 273: 260: 256: 253: 247: 244: 221: 220: 211: 210: 202: 201: 200: 199: 198: 196: 193: 142: 139: 137: 134: 77: 76: 31: 29: 22: 15: 9: 6: 4: 3: 2: 3935: 3924: 3921: 3919: 3916: 3915: 3913: 3899: 3895: 3891: 3887: 3883: 3882: 3874: 3866: 3862: 3858: 3854: 3847: 3840: 3821: 3814: 3807: 3803: 3791: 3787: 3786: 3781: 3777: 3770: 3766: 3759: 3754: 3753: 3745: 3742: 3741: 3735: 3733: 3728: 3726: 3722: 3718: 3717: 3706: 3704: 3695: 3691: 3687: 3681: 3665: 3660: 3656: 3654: 3646: 3641: 3632: 3630: 3625: 3621: 3617: 3607: 3605: 3599: 3587: 3582: 3578: 3576: 3575: 3569: 3568: 3561: 3543: 3540: 3539: 3533: 3530: 3529: 3523: 3520: 3519: 3512: 3509: 3508: 3505: 3475: 3469: 3464: 3460: 3456: 3453: 3448: 3441: 3438: 3432: 3429: 3423: 3420: 3411: 3406: 3401: 3399: 3391: 3388: 3385: 3379: 3371: 3365: 3361: 3358: 3352: 3349: 3345: 3341: 3338: 3335: 3333: 3325: 3319: 3308: 3307: 3306: 3302: 3295: 3284: 3273: 3260: 3256: 3252: 3235: 3227: 3214: 3206: 3197: 3191: 3187: 3186: 3171: 3168: 3167: 3161: 3158: 3157: 3151: 3148: 3147: 3141: 3138: 3137: 3130: 3127: 3126: 3123: 3100: 3095: 3090: 3087: 3082: 3077: 3074: 3071: 3051: 3048: 3045: 3042: 3039: 3031: 3030: 3029: 3012:. The factor 2997: 2993: 2989: 2985: 2979: 2977: 2973: 2968: 2964: 2947: 2939: 2926: 2918: 2909: 2903: 2899: 2898: 2890: 2882: 2877: 2871: 2858: 2855: 2854: 2848: 2845: 2844: 2838: 2835: 2834: 2828: 2825: 2824: 2818: 2814: 2811: 2810: 2807: 2795: 2790: 2776: 2769: 2766: 2762: 2759: 2752: 2747: 2742: 2739: 2734: 2728: 2725: 2721: 2717: 2712: 2709: 2704: 2700: 2694: 2690: 2687: 2684: 2664: 2661: 2657: 2654: 2650: 2647: 2638: 2636: 2632: 2628: 2610: 2602: 2591: 2583: 2572: 2564: 2530: 2526: 2520: 2516: 2510: 2507: 2502: 2499: 2496: 2489: 2488: 2487: 2485: 2473: 2469: 2465: 2449: 2440: 2409: 2406: 2399: 2395: 2391: 2386: 2382: 2375: 2372: 2369: 2364: 2361: 2352: 2351: 2350: 2348: 2317: 2311: 2308: 2305: 2302: 2295: 2287: 2284: 2278: 2272: 2269: 2266: 2260: 2255: 2251: 2245: 2242: 2235: 2234: 2233: 2216:at any point 2195: 2190: 2187: 2182: 2178: 2175: 2172: 2168: 2162: 2159: 2151: 2147: 2143: 2138: 2134: 2126: 2122: 2119: 2116: 2113: 2090: 2087: 2080: 2076: 2072: 2067: 2063: 2056: 2053: 2046: 2045: 2044: 2022: 2006: 1997: 1983: 1974: 1965: 1951: 1948: 1909: 1904: 1900: 1896: 1891: 1886: 1882: 1876: 1871: 1867: 1863: 1861: 1854: 1850: 1837: 1833: 1829: 1826: 1818: 1815: 1812: 1804: 1800: 1793: 1791: 1784: 1780: 1768: 1760: 1757: 1754: 1748: 1743: 1738: 1732: 1728: 1724: 1721: 1717: 1710: 1707: 1704: 1702: 1695: 1691: 1679: 1678: 1677: 1675: 1659: 1650: 1636: 1634: 1607: 1604: 1601: 1598: 1591: 1583: 1580: 1577: 1571: 1566: 1562: 1556: 1553: 1546: 1545: 1544: 1527:at any point 1504: 1501: 1494: 1490: 1486: 1481: 1477: 1470: 1467: 1460: 1459: 1458: 1452: 1447: 1444: 1440: 1436: 1432: 1416: 1407: 1396:Tangent ogive 1373: 1369: 1362: 1359: 1351: 1347: 1343: 1340: 1334: 1329: 1325: 1321: 1318: 1297: 1290: 1286: 1279: 1275: 1271: 1266: 1262: 1255: 1251: 1248: 1245: 1240: 1236: 1228: 1208: 1204: 1197: 1194: 1191: 1188: 1185: 1164: 1157: 1153: 1147: 1143: 1137: 1133: 1130: 1127: 1122: 1118: 1110: 1109: 1108: 1107: 1085: 1081: 1071: 1067: 1063: 1058: 1054: 1042: 1038: 1034: 1031: 1022: 1017: 1013: 1009: 1006: 986: 983: 980: 977: 972: 968: 959: 941: 937: 930: 926: 922: 916: 913: 891: 887: 883: 880: 877: 874: 866: 850: 846: 842: 837: 833: 829: 826: 819: 818: 817: 811: 802: 793: 788: 784: 776: 759: 750: 720: 716: 712: 707: 703: 699: 694: 690: 682: 681: 680: 652: 647: 643: 639: 634: 629: 625: 619: 614: 610: 606: 601: 597: 589: 588: 587: 577: 551: 547: 542: 538: 531: 526: 522: 514: 494: 490: 486: 481: 477: 470: 465: 461: 452: 447: 443: 437: 432: 428: 420: 419: 418: 416: 412: 396: 387: 355: 349: 346: 343: 340: 337: 316: 311: 308: 303: 299: 296: 293: 290: 283: 282: 281: 258: 254: 251: 245: 242: 235: 234: 233: 231: 215: 206: 192: 176: 133: 131: 127: 123: 119: 115: 111: 107: 103: 99: 95: 92: 83: 73: 70: 62: 52: 48: 42: 41: 35: 30: 21: 20: 3918:Aerodynamics 3880: 3873: 3856: 3852: 3839: 3827:. Retrieved 3820:the original 3806: 3784: 3769:the original 3764: 3729: 3724: 3721:aspect ratio 3720: 3714: 3712: 3699: 3669: 3649: 3613: 3601: 3571: 3566: 3559: 3556: 3499: 3300: 3293: 3282: 3271: 3248: 3233: 3212: 3181:Haack series 3117: 3020:above about 2995: 2991: 2987: 2983: 2980: 2966: 2963:power series 2962: 2960: 2945: 2924: 2893:Power series 2880: 2869: 2866: 2816: 2793: 2791: 2639: 2635:power series 2631:latus rectum 2624: 2608: 2589: 2570: 2482:, this is a 2461: 2335: 2224:varies from 2211: 2020: 2018: 1954:Secant ogive 1949: 1932: 1671: 1622: 1535:varies from 1522: 1451:ogive radius 1450: 1448: 1428: 1106:Half angles: 1105: 1104: 809: 800: 791: 786: 774: 771: 671: 578: 568: 408: 275: 227: 165:varies from 144: 88: 65: 56: 37: 3674:0.8 to Mach 3653:USAF Datcom 3620:wetted area 3572:Von Kármán 3128:Power type 2347:Honest John 1523:The radius 91:aerodynamic 51:introducing 3912:Categories 3798:References 3680:Von Kármán 3645:Boeing 737 3567:Von Kármán 3553:Von Kármán 3231:LV-Haack ( 3008:less than 2885:less than 2484:hemisphere 2429:Elliptical 1633:hemisphere 34:references 3898:253099252 3865:221684654 3732:wave drag 3664:transonic 3624:transonic 3592:Aerospike 3531:LV-Haack 3476:θ 3470:⁡ 3442:θ 3433:⁡ 3424:− 3421:θ 3412:π 3386:θ 3353:− 3342:⁡ 3320:θ 3139:Cylinder 3122:include: 3049:≤ 3043:≤ 2763:− 2722:− 2662:≤ 2651:≤ 2553:Parabolic 2511:− 2373:ρ 2318:α 2312:⁡ 2306:ρ 2303:− 2285:− 2279:α 2273:⁡ 2267:ρ 2261:− 2252:ρ 2179:⁡ 2173:− 2163:ρ 2123:⁡ 2114:α 2054:ρ 1897:− 1877:− 1830:− 1827:ρ 1816:− 1813:ρ 1758:− 1755:ρ 1749:− 1725:− 1722:ρ 1711:− 1608:ρ 1605:− 1581:− 1572:− 1563:ρ 1468:ρ 1370:ϕ 1363:⁡ 1344:− 1272:− 1252:⁡ 1237:ϕ 1205:ϕ 1198:⁡ 1134:⁡ 1119:ϕ 1064:− 1035:− 984:≤ 978:≤ 884:≤ 878:≤ 713:− 640:− 356:ϕ 350:⁡ 300:⁡ 291:ϕ 126:nose cone 98:nose cone 59:July 2018 3923:Rocketry 3890:60-15518 3829:11 April 3738:See also 3541:Tangent 3303:> 2/3 2972:cylinder 2770:′ 2729:′ 2677: : 2658:′ 2627:parabola 999: : 906: : 739:Bi-conic 110:aircraft 3725:caliber 3684:n = 1/2 2876:tangent 2592:′ = 3/4 2573:′ = 1/2 2478:equals 2468:prolate 2464:ellipse 1443:tangent 783:frustum 184:⁄ 114:missile 96:of the 47:improve 3896:  3888:  3863:  3676:  3672:  3516:value 3339:arccos 3134:value 2974:and a 2922:Half ( 2821:value 2606:Full ( 2568:Half ( 2342:ρ 2338:ρ 2176:arctan 2120:arccos 2025:ρ 1982:Secant 1933:where 1674:sphere 1629:ρ 1455:ρ 1439:circle 1249:arctan 1131:arctan 569:where 415:sphere 297:arctan 278:φ 122:bullet 106:rocket 94:design 36:, but 3861:S2CID 3849:(PDF) 3823:(PDF) 3816:(PDF) 3772:(PDF) 3761:(PDF) 3574:ogive 3296:= 2/3 3285:= 1/3 3236:= 1/3 3169:Cone 3032:For 2948:= 3/4 2927:= 1/2 2872:′ = 1 2856:Full 2836:Half 2826:Cone 2611:′ = 1 1531:, as 1431:ogive 195:Conic 161:, as 118:shell 3894:OCLC 3886:LCCN 3831:2011 3616:Mach 3255:drag 2976:cone 2961:The 2802:and 2640:For 2376:< 2370:< 2232:is: 2106:and 2057:> 2039:and 2031:and 1543:is: 1311:and 1178:and 960:For 867:For 330:and 230:cone 3655:). 3570:or 3562:= 0 3545:2/3 3535:1/3 3461:sin 3430:sin 3274:= 0 3215:= 0 3163:3/4 3153:1/2 3022:0.7 2850:3/4 2840:1/2 2309:sin 2270:cos 2228:to 2220:as 2021:not 1539:to 1360:tan 1195:tan 347:tan 120:or 108:or 3914:: 3892:. 3855:. 3851:. 3788:. 3763:. 3577:. 3289:LV 3287:, 3278:LD 3064:: 2986:= 2486:. 2349:. 1635:. 1453:, 816:. 280:: 116:, 112:, 3900:. 3867:. 3857:7 3833:. 3560:C 3525:0 3514:C 3502:C 3479:) 3473:( 3465:3 3457:C 3454:+ 3449:2 3445:) 3439:2 3436:( 3407:R 3402:= 3395:) 3392:C 3389:, 3383:( 3380:y 3372:) 3366:L 3362:x 3359:2 3350:1 3346:( 3336:= 3329:) 3326:x 3323:( 3301:C 3294:C 3283:C 3272:C 3267:C 3263:C 3238:) 3234:C 3217:) 3213:C 3173:1 3143:0 3132:n 3120:n 3101:n 3096:) 3091:L 3088:x 3083:( 3078:R 3075:= 3072:y 3052:1 3046:n 3040:0 3026:n 3018:n 3014:n 3010:1 3006:n 3002:x 2998:) 2996:L 2994:/ 2992:x 2990:( 2988:R 2984:y 2950:) 2946:n 2929:) 2925:n 2887:1 2883:′ 2881:K 2870:K 2860:1 2830:0 2819:′ 2817:K 2804:1 2800:0 2796:′ 2794:K 2777:) 2767:K 2760:2 2753:2 2748:) 2743:L 2740:x 2735:( 2726:K 2718:) 2713:L 2710:x 2705:( 2701:2 2695:( 2691:R 2688:= 2685:y 2665:1 2655:K 2648:0 2613:) 2609:K 2594:) 2590:K 2575:) 2571:K 2531:2 2527:L 2521:2 2517:x 2508:1 2503:R 2500:= 2497:y 2480:L 2476:R 2410:R 2407:2 2400:2 2396:L 2392:+ 2387:2 2383:R 2365:2 2362:L 2321:) 2315:( 2296:2 2292:) 2288:x 2282:) 2276:( 2264:( 2256:2 2246:= 2243:y 2230:L 2226:0 2222:x 2218:x 2214:y 2196:) 2191:L 2188:R 2183:( 2169:) 2160:2 2152:2 2148:R 2144:+ 2139:2 2135:L 2127:( 2117:= 2091:R 2088:2 2081:2 2077:L 2073:+ 2068:2 2064:R 2041:L 2037:R 2033:L 2029:R 1944:o 1942:x 1937:n 1935:r 1910:2 1905:t 1901:y 1892:2 1887:n 1883:r 1872:o 1868:x 1864:= 1855:t 1851:x 1838:n 1834:r 1822:) 1819:R 1810:( 1805:n 1801:r 1794:= 1785:t 1781:y 1769:2 1765:) 1761:R 1752:( 1744:2 1739:) 1733:n 1729:r 1718:( 1708:L 1705:= 1696:o 1692:x 1625:L 1602:R 1599:+ 1592:2 1588:) 1584:x 1578:L 1575:( 1567:2 1557:= 1554:y 1541:L 1537:0 1533:x 1529:x 1525:y 1505:R 1502:2 1495:2 1491:L 1487:+ 1482:2 1478:R 1471:= 1379:) 1374:2 1366:( 1357:) 1352:1 1348:L 1341:x 1338:( 1335:+ 1330:1 1326:R 1322:= 1319:y 1298:) 1291:2 1287:L 1280:1 1276:R 1267:2 1263:R 1256:( 1246:= 1241:2 1214:) 1209:1 1201:( 1192:x 1189:= 1186:y 1165:) 1158:1 1154:L 1148:1 1144:R 1138:( 1128:= 1123:1 1086:2 1082:L 1077:) 1072:1 1068:R 1059:2 1055:R 1051:( 1048:) 1043:1 1039:L 1032:x 1029:( 1023:+ 1018:1 1014:R 1010:= 1007:y 987:L 981:x 973:1 969:L 942:1 938:L 931:1 927:R 923:x 917:= 914:y 892:1 888:L 881:x 875:0 851:2 847:L 843:+ 838:1 834:L 830:= 827:L 813:2 810:R 804:1 801:R 795:2 792:L 778:1 775:L 721:n 717:r 708:o 704:x 700:= 695:a 691:x 676:a 674:x 653:2 648:t 644:y 635:2 630:n 626:r 620:+ 615:t 611:x 607:= 602:o 598:x 583:o 581:x 573:n 571:r 552:L 548:R 543:t 539:x 532:= 527:t 523:y 495:2 491:L 487:+ 482:2 478:R 471:2 466:n 462:r 453:R 448:2 444:L 438:= 433:t 429:x 359:) 353:( 344:x 341:= 338:y 317:) 312:L 309:R 304:( 294:= 259:L 255:R 252:x 246:= 243:y 187:L 181:C 171:L 167:0 163:x 159:x 155:y 151:R 147:L 72:) 66:( 61:) 57:( 43:.

Index

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Two-dimensional drawing of an elliptical nose cone with dimensions added to show how L is the total length of the nose cone, R is the radius at the base, and y is the radius at a point x distance from the tip.
aerodynamic
design
nose cone
compressible fluid
rocket
aircraft
missile
shell
bullet
nose cone
solid of revolution
body of revolution


cone


re-entry vehicles
sphere


frustum

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