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Volumn 2, Issue , 2005, Pages 775-785

Investigation of boundary layer bleed for improving scramjet isolator performance

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTER SIMULATION; JETS; SHOCK WAVES; TURBULENCE;

EID: 29044434887     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-3286     Document Type: Conference Paper
Times cited : (16)

References (13)
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    • (1992) AIAA Journal , vol.30 , Issue.2 , pp. 359-366
    • Morris, M.J.1    Sajben, M.2    Kroutil, J.C.3
  • 2
    • 0021937157 scopus 로고
    • Shock wave/turbulent boundary layer interaction and its control
    • Delery, J.M., "Shock Wave/Turbulent Boundary Layer Interaction and its Control," Progress in Aerospace Sciences, Vol. 22, 1985, pp. 209-280.
    • (1985) Progress in Aerospace Sciences , vol.22 , pp. 209-280
    • Delery, J.M.1
  • 5
    • 0027150227 scopus 로고
    • Shock/boundary-layer interaction control with vortex generators and passive cavity
    • McCormick, D. C., "Shock/Boundary-Layer Interaction Control with Vortex Generators and Passive Cavity," AIAA Journal, Vol.31, No. 1, 1993, pp.91-96.
    • (1993) AIAA Journal , vol.31 , Issue.1 , pp. 91-96
    • McCormick, D.C.1
  • 6
    • 35648973110 scopus 로고    scopus 로고
    • Control of normal shock wave/turbulent boundary-layer interaction using streamwise grooves
    • Smith, A. N., Babinsky, H., Fulker, J. L., and Ashill, P. A., "Control of Normal Shock Wave/Turbulent Boundary-Layer Interaction Using Streamwise Grooves," AIAA Paper 2002-0978, 2002.
    • (2002) AIAA Paper , vol.2002 , Issue.978
    • Smith, A.N.1    Babinsky, H.2    Fulker, J.L.3    Ashill, P.A.4
  • 7
    • 2342490268 scopus 로고    scopus 로고
    • Experiments on normal shock/boundary layer interaction control using aeroelastic mesoflaps
    • Hafenrichter, E. S., Lee, Y., McIlwain, S. T., Dutton, J. C., and Loth, E., "Experiments on Normal Shock/Boundary Layer Interaction Control Using Aeroelastic Mesoflaps," AIAA Paper 2001-0156, 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.156
    • Hafenrichter, E.S.1    Lee, Y.2    McIlwain, S.T.3    Dutton, J.C.4    Loth, E.5
  • 8
    • 74549151469 scopus 로고    scopus 로고
    • Numerical analysis of streamline-traced hypersonic Inlets
    • Tam, C.-J., Baurle, R.A., and Streby, G.D., "Numerical Analysis of Streamline-Traced Hypersonic Inlets," AIAA Paper 2003-0013, 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.13
    • Tam, C.-J.1    Baurle, R.A.2    Streby, G.D.3
  • 9
    • 29044449782 scopus 로고    scopus 로고
    • Mach 4 performance of a fixed-geometry hypersonic inlet with rectangular-to-elliptical shape transition
    • Smart, M. K., and Trexler, C. A., "Mach 4 Performance of a Fixed-Geometry Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition," AIAA Paper 2003-0012, 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.12
    • Smart, M.K.1    Trexler, C.A.2
  • 10
    • 0013121698 scopus 로고    scopus 로고
    • A pseudo-temporal multi-grid relaxation scheme for solving the parabolized navier-stokes equations
    • White, J. and Morrison, J.H., "A Pseudo-Temporal Multi-Grid Relaxation Scheme for Solving the Parabolized Navier-Stokes Equations," AIAA Paper 1999-3360, 1999.
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    • White, J.1    Morrison, J.H.2
  • 12
    • 0031190973 scopus 로고    scopus 로고
    • A low-diffusion flux-splitting scheme for navier-stokes calculations
    • Edwards, J.R., "A Low-Diffusion Flux-Splitting Scheme for Navier-Stokes Calculations," Computers & Fluids, Vol. 26, No. 6, 1997, pp. 635-659.
    • (1997) Computers & Fluids , vol.26 , Issue.6 , pp. 635-659
    • Edwards, J.R.1
  • 13
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    • Zonal two equation κ-ω models for aerodynamic flows
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    • Menter, F.R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.