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0002603384
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Preliminary investigations of spiked bodies at hypersonic speeds
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Bogdonoff, S. M., and Vas, E. I., "Preliminary Investigations of Spiked Bodies at Hypersonic Speeds," Journal of the Aeronautical Sciences, Vol. 26, No. 2, 1959, pp. 65-74.
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Bogdonoff, S.M.1
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3
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0026190038
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Spike-nosed projectiles: Computations and dual flow modes in supersonic flight
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July-August
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Mikhail, A.G. "Spike-Nosed Projectiles: computations and Dual Flow Modes in Supersonic Flight," Journal of Spacecraft and Rockets, Vol. 28, No. 4, July-August1991, pp. 418-424.
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Mikhail, A.G.1
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4
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0029678841
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Spike-nosed projectiles with vortex rings: Steady and nonsteady flow simulations
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January-February
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Mikhail, A.G. "Spike-Nosed Projectiles with Vortex Rings: Steady and Nonsteady Flow Simulations," Journal of Spacecraft and Rockets, Vol. 33, No. 1, January-February1996, pp. 8-15.
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Mikhail, A.G.1
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5
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Unsteady aerodynamic considerations in the design of a drag-reduction spike
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January
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Reding J. P., Guenther, R. A., and Richter, B. J. "Unsteady Aerodynamic Considerations in the Design of a Drag-Reduction Spike," Journal of Spacecraft and Rockets, Vol. 14, No. 1, January 1977, pp. 54-60.
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Reding, J.P.1
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6
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0018995709
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Scale effects on fluctuating pressures in spike-induced flow separation
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January
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Reding J. P., Guenther, R. A., and Richter, B. J. "Scale Effects on Fluctuating Pressures in Spike-Induced Flow Separation," Journal of Spacecraft and Rockets, Vol. 14, No. 1, January 1977, pp. 112-118.
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Reding, J.P.1
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Richter, B.J.3
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7
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0017015449
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Asymmetric shock-wave oscillations on spiked bodies of revolution
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Demetriades A., and Hopkins, A. T. (Lt.), "Asymmetric Shock-Wave Oscillations on Spiked Bodies of Revolution," Journal of Spacecraft and Rockets, Vol. 13, No. 11, 1976, pp. 703-704.
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Demetriades, A.1
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9
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0345714800
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Shock tunnel high speed photography and CFD calculations on spiketipped bodies
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Srulijes, J., Gnemmi, P., Seiler, F., and Runne, K., "Shock tunnel high speed photography and CFD calculations on spiketipped bodies," Proceedings of SPIE, Vol. 4948, 2003, pp. 658-670.
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Srulijes, J.1
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10
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0142023856
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Experimental investigations of hypersonic flow over highly blunted cones with aerospikes
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October
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Menezes, V., Saravanan, S., Jagadeesh, G., and Reddy K. P. J., "Experimental Investigations of Hypersonic Flow over Highly Blunted Cones with Aerospikes," AIAA Journal, Vol. 41, No. 10, October 2003, pp. 1955-1966.
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Menezes, V.1
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11
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0029197324
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Numerical investigation of supersonic flows around a spiked blunt body
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January-February 19
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Yamauchi M., Fujii, K., and Higashino, F. "Numerical Investigation of Supersonic Flows Around a Spiked Blunt Body," Journal of Spacecraft and Rockets, Vol. 32, No. 1, January-February 19, pp. 33-42.
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12
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0142180025
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Flowfield around spike-tipped bodies for high attack angles at Mach 4.5
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September-October
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Gnemmi, P., Srulijes, J. and Roussel, K. "Flowfield Around Spike-Tipped Bodies for High Attack Angles at Mach 4.5," Journal of Spacecraft and Rockets, Vol. 40, No. 5, September-October 2003, pp. 622-631.
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Gnemmi, P.1
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14
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0020810471
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Effects of external burning on spike-induced separated flow
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Sept-Oct
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Reding J. P., and Jecmen, D. M. "Effects of External Burning on Spike-Induced Separated Flow," Journal of Spacecraft and Rockets, Vol. 20, No. 5, Sept-Oct 1983, pp. 452-453.
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Reding, J.P.1
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15
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AIAA Paper 96-3143, June
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Diaz, E., Toro, P. G. P., Myrabo, L. N., Nagamatsu, H. T., and Messitt, D. G., "Experimental Pressure Survey of the Hypersonic Air Spike Inlet at Mach 10," AIAA Paper 96-3143, June 1996.
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Experimental Pressure Survey of the Hypersonic Air Spike Inlet at Mach 10
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Diaz, E.1
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Nagamatsu, H.T.4
Messitt, D.G.5
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84983175032
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AIAA Paper 97-795, January
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Toro, P. G. P., Myrabo, L. N., and Nagamatsu, H. T., "Experimental Investigation of Hypersonic "Directed-Energy Air Spike" inlet at Mach 10-20," AIAA Paper 97-795, January 1997.
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Experimental Investigation of Hypersonic "Directed-Energy Air Spike" Inlet at Mach 10-20
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Toro, P.G.P.1
Myrabo, L.N.2
Nagamatsu, H.T.3
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18
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4243763832
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AIAA Paper 95-0737
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Huebner, D. L., Mitchell, A. M., and Bodreaux, E. J., "Experimental Results on the Feasibility of an Aerospike for Hypersonic Missiles," AIAA Paper 95-0737.
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Experimental Results on the Feasibility of an Aerospike for Hypersonic Missiles
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Huebner, D.L.1
Mitchell, A.M.2
Bodreaux, E.J.3
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19
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78549289283
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Numerical heat transfer study over spike blunt bodies at mach 6.8
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July-August
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Mehta, R.C. "Numerical Heat Transfer Study over Spike Blunt Bodies at Mach 6.8," Journal of Spacecraft and Rockets, Vol. 37, No. 5, July-August1991, pp. 418-424.
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Mehta, R.C.1
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