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Volumn 20, Issue 5, 2005, Pages 731-735

Unstart simulation of scramjet inlets

Author keywords

Aerospace propulsion system; Inlet; Judgement criterion; Scramjet; Unstart

Indexed keywords

ANGLE OF ATTACK INDICATORS; COMPUTER SIMULATION; PRESSURE DISTRIBUTION; RAMJET ENGINES; SHOCK WAVES; STEADY FLOW; TWO DIMENSIONAL;

EID: 28244489321     PISSN: 10008055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (12)

References (8)
  • 1
    • 28244445087 scopus 로고    scopus 로고
    • Chinese source
  • 2
    • 0004305118 scopus 로고    scopus 로고
    • CIAM/NASA mach scramjet flight and ground test
    • AIAA-99-4848
    • Voland R T, Auslender A H. CIAM/NASA Mach Scramjet flight and ground test[R]. AIAA-99-4848.
    • Voland, R.T.1    Auslender, A.H.2
  • 3
    • 0035552112 scopus 로고    scopus 로고
    • Experiment study on supersonic inlet in dual-model scramjet
    • Yang Jin-jun, Zhang Kun-yuan, Xu Hui, Xu Jing-lei. Experiment Study on Supersonic Inlet in Dual-Model Scramjet [J]. Journal of Propulsion Technology, 2001, 22(6): 473-475.
    • (2001) Journal of Propulsion Technology , vol.22 , Issue.6 , pp. 473-475
    • Yang, J.-J.1    Zhang, K.-Y.2    Xu, H.3    Xu, J.-L.4
  • 4
    • 0036700175 scopus 로고    scopus 로고
    • Investigation of flow in isolator of hypersonic inlet
    • Zhang Kun-yuan, Wang Cheng-peng, Yang Jian-jun. Investigation of Flow in Isolator of Hypersonic Inlet [J]. Journal of Propulsion Technology, 2002, 23(4): 311-314.
    • (2002) Journal of Propulsion Technology , vol.23 , Issue.4 , pp. 311-314
    • Zhang, K.-Y.1    Wang, C.-P.2    Yang, J.-J.3
  • 5
    • 12744275710 scopus 로고    scopus 로고
    • Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a mach number of 4
    • Saied Emami, Carl A Trexler. Experimental Investigation of Inlet-Combustor Isolators for a Dual-Mode Scramjet at a Mach Number of 4[R]. NASA Technical Paper 3502.
    • NASA Technical Paper 3502
    • Emami, S.1    Trexler, C.A.2
  • 6
    • 0036812333 scopus 로고    scopus 로고
    • Numerical study of mach number at the 3-D sidewall compression hypersonic inlet and isolator
    • Xu Jing-lei, Zhang Kun-yuan, Ling Wen-hui. Numerical Study of Mach Number at the 3-D Sidewall Compression Hypersonic Inlet and Isolator[J]. Journal of Aerospace Power, 2002, 17(4): 489-494.
    • (2002) Journal of Aerospace Power , vol.17 , Issue.4 , pp. 489-494
    • Xu, J.-L.1    Zhang, K.-Y.2    Ling, W.-H.3
  • 7
    • 28244486640 scopus 로고    scopus 로고
    • Two-dimensional viscous simulation of a inlet-isolator flows at mach number 4
    • AIAA 01-34513
    • Ding M, Hua L, Xiao F Qiang. Two-Dimensional Viscous Simulation of a Inlet-isolator flows at Mach Number 4[R]. AIAA 01-34513.
    • Ding, M.1    Hua, L.2    Xiao, F.Q.3
  • 8
    • 0011783527 scopus 로고    scopus 로고
    • Fluent Inc., Lebanon
    • Fluent 6.0 User's Guide[Z]. Fluent Inc., Lebanon, 2001.
    • (2001) Fluent 6.0 User's Guide


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.