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Volumn 28, Issue 6, 2007, Pages 1488-1493

Experimental investigation of inlet start/unstart influences on the aerodynamic characteristic of a hypersonic vehicle

Author keywords

Airframe engine integrated; Hypersonic vehicle; Inlet; Lift drag ratio; Start unstart

Indexed keywords

AIRCRAFT; AIRFRAMES; DRAG; FLOW PATTERNS; LIFT; MACH NUMBER; SHOCK WAVES;

EID: 34447310375     PISSN: 10001328     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (11)

References (10)
  • 1
    • 40749098332 scopus 로고    scopus 로고
    • Optimization of airbreathing propulsion system for the TSTO spaceplane
    • AIAA, 2001-1912S
    • Hiroald Kobyashi, Telsuya Sato, Nobuhiro Tanataugu. Optimization of airbreathing propulsion system for the TSTO spaceplane[R]. AIAA, 2001-1912
    • Kobyashi, H.1    Sato, T.2    Tanataugu, N.3
  • 2
    • 40749109599 scopus 로고    scopus 로고
    • An integrated optimization for conceptual designs of airbreathing launch TSTO vehicle
    • AIAA, 2001-1902
    • Tsuchiya T, Mori T, Maita M. An integrated optimization for conceptual designs of airbreathing launch TSTO vehicle[R]. AIAA, 2001-1902
    • Tsuchiya, T.1    Mori, T.2    Maita, M.3
  • 3
    • 0035389997 scopus 로고    scopus 로고
    • Critical design issues for airbreathing hypersonic waverider missiles
    • Ryan P, Starkey Mark, Lewis J. Critical design issues for airbreathing hypersonic waverider missiles[J]. Journal of Spacecr4jt and Rockets, 2001, 38(4): 510-519
    • (2001) Journal of Spacecr4jt and Rockets , vol.38 , Issue.4 , pp. 510-519
    • Ryan, P.1    Mark, S.2    Lewis, J.3
  • 4
    • 40749109197 scopus 로고    scopus 로고
    • Integrated propulsion effects on dynamic stability and control of hypersonic watersides
    • AIAA, 2000-3826, Taskinoglu E.S. and Knight D., Numerical Analysis of Submerged Inlets, AIAA 2002-3147
    • von Eggers Lael, Rudd Darryll, Pines J. Integrated propulsion effects on dynamic stability and control of hypersonic watersides[R]. AIAA, 2000-3826. Ezgi S. Taskinoglu, Doyle Knight. Numerical Analysis of Submerged Inlets, AIAA 2002-3147
    • von Lael, E.1    Darryll, R.2    Pines, J.3
  • 5
    • 34547996101 scopus 로고    scopus 로고
    • Characteristics of shock train in two dimensional bends with constant area
    • TAN Hui-jun, GUO Rong-wei. Characteristics of shock train in two dimensional bends with constant area[J]. Acta Aeroddynamica Sinica, 2007, 28(4): 783-790
    • (2007) Acta Aeroddynamica Sinica , vol.28 , Issue.4 , pp. 783-790
    • Tan, H.-J.1    Guo, R.-W.2
  • 6
    • 36249005248 scopus 로고    scopus 로고
    • Numerical study of airframe/propulsion integrative hypersonic vehicle
    • China Aerodynamics Research and Development Center Graduate School
    • HE Yuan-yuan. Numerical study of airframe/propulsion integrative hypersonic vehicle[D]. China Aerodynamics Research and Development Center Graduate School, 2004, 10
    • (2004) , pp. 10
    • He, Y.-Y.1
  • 7
    • 12744275710 scopus 로고    scopus 로고
    • Experimental investigation of inlet-combustor isolators for a dual-mode seramjet at a mach number of 4
    • NASA-TP-3502
    • Emami, Trexler A, Auslender H, Weidner P. Experimental Investigation of Inlet-Combustor Isolators for a Dual-Mode Seramjet at a Mach Number of 4[R]. NASA-TP-3502
    • Emami1    Trexler, A.2    Auslender, H.3    Weidner, P.4
  • 8
    • 12744256388 scopus 로고    scopus 로고
    • Wind-tunnel blockage and actuation systems test of a two-dimensional seramjet inlet unstart model at mach 6
    • NASA-TM-109152
    • Wind-Tunnel Blockage and Actuation Systems Test of a Two-Dimensional Seramjet Inlet Unstart Model at Mach 6[R]. NASA-TM-109152
  • 9
    • 0005417237 scopus 로고    scopus 로고
    • Starting characteristics of supersonic inlets
    • AIAA-96-2914
    • Van Wie D M, Kwok F T, Walsh R F. Starting characteristics of supersonic inlets[R]. AIAA-96-2914, 1996
    • (1996)
    • van Wie, D.M.1    Kwok, F.T.2    Walsh, R.F.3
  • 10
    • 34447334005 scopus 로고    scopus 로고
    • Experimental study of the unstable-unstarted condition of a hypersonic inlet at mach 6
    • TAN Hui-jun, GUO Rong-wei. Experimental study of the unstable-unstarted condition of a hypersonic inlet at mach 6[J]. AIAA Journal of Propulsion and Power, 2007, 23(4): 543-548
    • (2007) AIAA Journal of Propulsion and Power , vol.23 , Issue.4 , pp. 543-548
    • Tan, H.-J.1    Guo, R.-W.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.