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Volumn 100, Issue 996, 1996, Pages 197-208

Hypersonic control flap effectiveness

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; DEFLECTION (STRUCTURES); HEAT TRANSFER; HIGH SPEED PHOTOGRAPHY; JET FLAPS; LIQUID CRYSTALS; PLATES (STRUCTURAL COMPONENTS); PRESSURE MEASUREMENT; REYNOLDS NUMBER; SCHLIEREN SYSTEMS; SURFACES; THERMAL VARIABLES MEASUREMENT;

EID: 0030171142     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article
Times cited : (8)

References (21)
  • 2
    • 0024088491 scopus 로고
    • Effects of nose bluntness and cone angle on slender vehicle transition
    • October
    • ERICSSON, L.E. Effects of nose bluntness and cone angle on slender vehicle transition, AIAA J, October 1988, 26, (10).
    • (1988) AIAA J , vol.26 , Issue.10
    • Ericsson, L.E.1
  • 4
    • 0004352688 scopus 로고
    • Stability of a laminar boundary layer on a blunted flat plate in supersonic flow-laminar-turbulent transition
    • Stuttgart, September
    • RESHOTKO, E. and KHAN, M.M.S. Stability of a laminar boundary layer on a blunted flat plate in supersonic flow-laminar-turbulent transition, IUTAM Symposium, Stuttgart, September 1979, pp 189-200.
    • (1979) IUTAM Symposium , pp. 189-200
    • Reshotko, E.1    Khan, M.M.S.2
  • 9
    • 0342688936 scopus 로고
    • Experiments on shockwave-boundary layer interaction at high Mach number with entropy layer effect
    • Marseille
    • COET, M.C., DELERY, J. and CHANTEZ, B. Experiments on shockwave-boundary layer interaction at high Mach number with entropy layer effect, IUTAM Symposium, Marseille, 1992.
    • (1992) IUTAM Symposium
    • Coet, M.C.1    Delery, J.2    Chantez, B.3
  • 11
    • 0016569867 scopus 로고
    • A correlation between pressure and heat transfer distributions at supersonic and hypersonic speeds
    • Nov
    • STOLLERY, J.L. and COLEMAN, G.T. A correlation between pressure and heat transfer distributions at supersonic and hypersonic speeds, Aeronaut Q, Nov 1975, 26, (5), pp 304-312.
    • (1975) Aeronaut Q , vol.26 , Issue.5 , pp. 304-312
    • Stollery, J.L.1    Coleman, G.T.2
  • 12
    • 6144228988 scopus 로고    scopus 로고
    • AMES RESEARCH STAFF Equations, tables and charts for compressible flows, NACA-R-1135, 1953
    • AMES RESEARCH STAFF Equations, tables and charts for compressible flows, NACA-R-1135, 1953.
  • 13
    • 6144240977 scopus 로고
    • The effect of leading edge bluntness on control effectiveness at hypersonic speeds
    • July 1993, Marseille
    • KUMAR, D. and STOLLERY, J.L. The effect of leading edge bluntness on control effectiveness at hypersonic speeds, 19th International Symposium on Shock Waves, July 1993, Marseille, 1993.
    • (1993) 19th International Symposium on Shock Waves
    • Kumar, D.1    Stollery, J.L.2
  • 17
    • 0007653181 scopus 로고
    • Turbulent hypersonic flow at a wedge-compression corner
    • ELFSTROM, G.M. Turbulent hypersonic flow at a wedge-compression corner, J Fluid Mech, 1972, 53, (1), PP 113-127.
    • (1972) J Fluid Mech , vol.53 , Issue.1 , pp. 113-127
    • Elfstrom, G.M.1
  • 19
    • 0007718077 scopus 로고
    • PhD thesis, University of London, See also NEEDHAM and STOLLERY AIAA Paper 66-455
    • NEEDHAM, D.A. Laminar Separation in Hypersonic Flows, PhD thesis, University of London, 1965. (See also NEEDHAM and STOLLERY AIAA Paper 66-455, 1966).
    • (1965) Laminar Separation in Hypersonic Flows
    • Needham, D.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.