Thermal protection and drag reduction with use of spike in hypersonic flow

10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2001, Pages

  Motoyama, Noboru ^a   Mihara, Ken ^a   Miyajima, Ryo ^a   Watanuki, Tadaharu ^a   Kubota, Hirotoshi ^a  

^a UNIVERSITY OF TOKYO   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894306129     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Crawford, D. H., Investigation of the flow over spiked-nose hemisphere-cylinder at Mach number of 6.8, NASA TN D-118 (1959).
2. Zorea, C. and Rom, J., Effect of a spike on the drag and on the aerodynamic stability of blunt bodies in supersonic flow, Journal of Spacecraft, Vol. 7, No. 8, pp. 1017-1019(1970).
3. Fujita, M. and Kubota, H., Numerical simulation of flow field over a spiked-nose, Computational Fluid Dynamics Journal, Vol. 1, No. 2, pp. 187-195 (1992).
4. Huebner, L. D., Experimental results on the feasibility of an aerospike for hypersonic missiles, AIAA Paper 95-0737 (1995).
5. Kijima, M, Kubota, H., Watanuki, T. and Fujita, M., Effect of nose configuration of spike on reduction of pressure drag in hypersonic flow, AAS 95-582, Advances in the Astronautical Sciences, pp. 273-284 (1996).
6. Sakagoshi, A., Mihara, K., Yamamoto, M, Watanuki, T. and Kubota, H., Effectiveness of an Aerospike for Reduction of Hypersonic Aerodynamic Heating, ISTS, 2000-e-23 (2000).
7. Nutt, K. W., Measurement technique for hypersonic flows, von Karman Institute for Fluid Dynamics (1990).
8. Lees, L., Laminar heat transfer over blunt-nosed bodies at hypersonic flight speeds, Jet Propulsion, Vol. 26, pp. 259-269 (1956).
9. Hayes, W. D. and Probstein, R. E, Hypersonic flow theory, Vol. 1, Inviscid folws, Academic Press (1966).