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Volumn , Issue 563, 2004, Pages 553-558

Study on aerothermal effects of viscous shock interaction in hypersonic inlets

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; ORBITS; PRESSURE MEASUREMENT; SPACE APPLICATIONS; THERMAL LOAD;

EID: 23844477947     PISSN: 03796566     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (21)

References (10)
  • 1
    • 0003922125 scopus 로고
    • Computational fluid mechanics and heat transfer
    • Minkowycz, W. J. and Sparrow, E. M. (eds.), Hemisphere Publishing Corporation, New York
    • Anderson, D. A., et al., Computational Fluid Mechanics and Heat Transfer, Series in Computational Methods in Mechanics and Thermal Sciences, Minkowycz, W. J. and Sparrow, E. M. (eds.), Hemisphere Publishing Corporation, New York, 1984.
    • (1984) Series in Computational Methods in Mechanics and Thermal Sciences
    • Anderson, D.A.1
  • 2
    • 84896692994 scopus 로고    scopus 로고
    • Finite volume numerical methods for aeroheating rate calculations from infrared thermographic data
    • Paper 2003-3634 presented on the, Orlando, FL
    • th AIAA Thermophysics Conf., Orlando, FL, 2003.
    • (2003) th AIAA Thermophysics Conf.
    • Daryabeigi, K.1
  • 4
    • 0037347735 scopus 로고    scopus 로고
    • Structure of flow over a hypersonic inlet with side compression wedges
    • Goonko, Y. P., et al., Structure of Flow over a Hypersonic Inlet with Side Compression Wedges, AIAA Journal, Vol. 41, No. 3, 436-447, 2003.
    • (2003) AIAA Journal , vol.41 , Issue.3 , pp. 436-447
    • Goonko, Y.P.1
  • 5
    • 33645360410 scopus 로고    scopus 로고
    • Survey on experimental studies of viscous interaction effects in hypersonic inlets at DLR cologne
    • to be published by Wiley
    • Henckels A. and Gruhn P., Survey on Experimental Studies of Viscous Interaction Effects in Hypersonic Inlets at DLR Cologne, "Basic Research Technologies for Two-Stage-to-Orbit Vehicles", to be published by Wiley.
    • Basic Research Technologies for Two-stage-to-orbit Vehicles
    • Henckels, A.1    Gruhn, P.2
  • 7
    • 33645349719 scopus 로고    scopus 로고
    • Der Hyperschallwindkanal H2K des DLR in Köln-Porz (Stand 2000)
    • Köln
    • Niezgodka F.-J., Der Hyperschallwindkanal H2K des DLR in Köln-Porz (Stand 2000), DLR-Mitteilung 2001-01, Köln 2002.
    • (2002) DLR-mitteilung 2001-01
    • Niezgodka, F.-J.1
  • 8
    • 33645333540 scopus 로고    scopus 로고
    • Experimental investigation of a hypersonic inlet for the TSTO-configuration ELAC
    • "New Results in Numerical and Experimental Fluid Mechanics III", ed. S. Wagner et al., Springer
    • Neubacher R., et al., Experimental Investigation of a Hypersonic Inlet for the TSTO-Configuration ELAC, "New Results in Numerical and Experimental Fluid Mechanics III", ed. S. Wagner et al., in "Notes on Numerical Fluid Mechanics, Vol. 77, 129-136, Springer, 2002.
    • (2002) Notes on Numerical Fluid Mechanics , vol.77 , pp. 129-136
    • Neubacher, R.1
  • 9
    • 0346098230 scopus 로고    scopus 로고
    • Reduction of shock induced boundary layer separation in hypersonic inlets using bleed
    • Elsevier, Paris
    • Schulte D., et al., Reduction of Shock Induced Boundary Layer Separation in Hypersonic Inlets Using Bleed,. Aerospace Science and Technology, Vol. 2, No. 4, pp. 231-239, Elsevier, Paris, 1998.
    • (1998) Aerospace Science and Technology , vol.2 , Issue.4 , pp. 231-239
    • Schulte, D.1
  • 10
    • 0035332672 scopus 로고    scopus 로고
    • Manipulation of shock/boundary layer interactions in hypersonic inlets
    • Schulte D., et al., Manipulation of Shock/Boundary Layer Interactions in Hypersonic Inlets, AIAA Journal of Propulsion and Power, Vol. 17, No. 3, 585-590, 2001.
    • (2001) AIAA Journal of Propulsion and Power , vol.17 , Issue.3 , pp. 585-590
    • Schulte, D.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.