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Volumn 34, Issue 6, 1997, Pages 762-768

Control effectiveness of a Jet-Slender body combination at hypersonic speeds

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; CONES; FLOW CONTROL; FORCE MEASUREMENT; JETS; MISSILES; PRESSURE MEASUREMENT; REYNOLDS NUMBER; SPEED;

EID: 0031273929     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3283     Document Type: Article
Times cited : (34)

References (19)
  • 3
    • 0013414350 scopus 로고
    • Swept Shock-Wave/Boundary-Layer Interactions
    • edited by M. J. Hemsch, Progress in Astronautics and Aeronautics, AIAA, Washington, DC
    • Settles, G. S., and Dolling, D. S., "Swept Shock-Wave/Boundary-Layer Interactions," Tactical Missile Aerodynamics: General Topics, edited by M. J. Hemsch, Vol. 141, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1992, pp. 505-574.
    • (1992) Tactical Missile Aerodynamics: General Topics , vol.141 , pp. 505-574
    • Settles, G.S.1    Dolling, D.S.2
  • 5
    • 3943095365 scopus 로고
    • Hypersonic Interactions about a Slender Cone Induced by Radial Mass Injection
    • AGARD CP-30
    • Simpkins, P., "Hypersonic Interactions About a Slender Cone Induced by Radial Mass Injection," Hypersonic Boundary Layers and Flow Fields, AGARD CP-30, 1968.
    • (1968) Hypersonic Boundary Layers and Flow Fields
    • Simpkins, P.1
  • 6
    • 0007688539 scopus 로고
    • Ph.D. Thesis, Dept. of Aerospace Sciences, Cranfield Univ., Bedfordshire, England, UK, Jan.
    • Kumar, D., "Hypersonic Control Effectiveness," Ph.D. Thesis, Dept. of Aerospace Sciences, Cranfield Univ., Bedfordshire, England, UK, Jan. 1995.
    • (1995) Hypersonic Control Effectiveness
    • Kumar, D.1
  • 12
    • 0009442298 scopus 로고
    • Boundary Layer Displacement and Leading Edge Bluntness Effects in High Temperature Hypersonic Flow
    • Cheng, H. K., Hall, J. G., Golian, T. C., and Hertzberg, A., "Boundary Layer Displacement and Leading Edge Bluntness Effects in High Temperature Hypersonic Flow," Journal of the Aerospace Sciences, Vol. 28, No. 5, 1961, pp. 353-381.
    • (1961) Journal of the Aerospace Sciences , vol.28 , Issue.5 , pp. 353-381
    • Cheng, H.K.1    Hall, J.G.2    Golian, T.C.3    Hertzberg, A.4
  • 14
    • 84940077375 scopus 로고
    • Cone Pressure Distribution at Large and Small Angles of Attack
    • High, W., and Blick, E., "Cone Pressure Distribution at Large and Small Angles of Attack," AIAA Journal, Vol. 2, No. 11, 1964, pp. 2054, 2055.
    • (1964) AIAA Journal , vol.2 , Issue.11 , pp. 2054
    • High, W.1    Blick, E.2
  • 15
    • 85081467119 scopus 로고
    • M.S. Thesis, Dept. of Aerospace Sciences, Cranfield Univ., Bedfordshire, England, UK, Aug.
    • Kontis, K., "Control by Blowing at Hypersonic Speeds," M.S. Thesis, Dept. of Aerospace Sciences, Cranfield Univ., Bedfordshire, England, UK, Aug. 1994.
    • (1994) Control by Blowing at Hypersonic Speeds
    • Kontis, K.1
  • 17
    • 0026867287 scopus 로고
    • Basic Experiments on a Supersonic Vortex Flow Around a Missile Body
    • Pagan, D., Molton, P., and Delery, J., "Basic Experiments on a Supersonic Vortex Flow Around a Missile Body," Journal of Spacecraft and Rockets, Vol. 29, No. 3, 1992, pp. 373-378.
    • (1992) Journal of Spacecraft and Rockets , vol.29 , Issue.3 , pp. 373-378
    • Pagan, D.1    Molton, P.2    Delery, J.3
  • 19
    • 85007670985 scopus 로고
    • Secondary Injection of Gases into a Supersonic Flow
    • Zukoski, E., and Spaid, F., "Secondary Injection of Gases into a Supersonic Flow," AIAA Journal, Vol. 2, No. 10, 1964, pp. 1689-1696.
    • (1964) AIAA Journal , vol.2 , Issue.10 , pp. 1689-1696
    • Zukoski, E.1    Spaid, F.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.