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Volumn 110, Issue 1108, 2006, Pages 353-360

Comparison of experimental and numerical investigation on a jet in a supersonic cross-flow

Author keywords

[No Author keywords available]

Indexed keywords

AIR EJECTORS; DATA REDUCTION; NUMBER THEORY; PRESSURE EFFECTS; REYNOLDS NUMBER; SUPERSONIC FLOW;

EID: 33745784146     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000001263     Document Type: Article
Times cited : (13)

References (14)
  • 1
    • 0003589601 scopus 로고
    • Fifty years of jet in cross flow research
    • AGARD-CP-534, Computational and Experimental Assessment of Jets in Cross Flow, UK, 19-22 April
    • MARGASON, R.J. Fifty years of jet in cross flow research, AGARD-CP-534, Computational and Experimental Assessment of Jets in Cross Flow, Symp. In Winchester, UK, 19-22 April 1993.
    • (1993) Symp. In Winchester
    • Margason, R.J.1
  • 2
    • 33745770948 scopus 로고
    • Experimentelle untersuchungen an festen spoilern und strahlspoilern bei machschen zahlen von 0.6 bis 2.8
    • HEYSER, A. and MAURER, F. Experimentelle Untersuchungen an festen Spoilern und Strahlspoilern bei Machschen Zahlen von 0.6 bis 2.8, Z. flugwiss. 1962, 10, Heft 4/5, S. 110-130.
    • (1962) Z. Flugwiss. , vol.10 , Issue.4-5 , pp. 110-130
    • Heyser, A.1    Maurer, F.2
  • 3
    • 85007691353 scopus 로고
    • A study of the interaction of gaseous jets from transverse slots with supersonic external flows
    • SPAID, F.W. and ZUKOSKI, E.E. A study of the interaction of gaseous jets from transverse slots with supersonic external flows, AIAA J, 1966, 6, (2), pp 205-212
    • (1966) AIAA J , vol.6 , Issue.2 , pp. 205-212
    • Spaid, F.W.1    Zukoski, E.E.2
  • 4
    • 0039436791 scopus 로고
    • Der Rohrwindkanal der aerodynamischen Versuchsanstalt Göttingen, Germany
    • LUDWIEG, H., HOTTNER, TH. and GRAUER-CARSTENSEN, H. Der Rohrwindkanal der aerodynamischen Versuchsanstalt Göttingen, Germany. Jahrbuch der DGLR, 1969, S. pp 52-58.
    • (1969) Jahrbuch der DGLR , pp. 52-58
    • Ludwieg, H.1    Hottner, Th.2    Grauer-Carstensen, H.3
  • 5
    • 0011906123 scopus 로고    scopus 로고
    • Documentation of experimental data for hypersonic 3-D shock waves/turbulent boundary layer interaction flows
    • DLR, Göttingen, Germany
    • SCHÜLEIN, E. and ZHELTOVODOV, A. Documentation of experimental data for hypersonic 3-D shock waves/turbulent boundary layer interaction flows, 2001, internal report IB 223-99 A 26, DLR, Göttingen, Germany.
    • (2001) Internal Report , vol.IB 223-99 A 26
    • Schülein, E.1    Zheltovodov, A.2
  • 6
    • 0012610538 scopus 로고    scopus 로고
    • Efficient computation of 3D-flows for complex configurations with the DLR TAU-Code using automatic adaptation
    • Vieweg
    • GERHOLD, T. and EVANS, J. Efficient computation of 3D-flows for complex configurations with the DLR TAU-Code using automatic adaptation, Notes on Numerical Fluid Mechanics, 1999, 72, Vieweg.
    • (1999) Notes on Numerical Fluid Mechanics , vol.72
    • Gerhold, T.1    Evans, J.2
  • 8
    • 0003471394 scopus 로고
    • A one-equation turbulence model for aerodynamic flows
    • 6-9 January Reno, USA, AIAA-92-0439
    • SPALART, P.R. and ALLMARAS, S.R. A one-equation turbulence model for aerodynamic flows, 30th Aerospace Sciences Meeting & Exhibit, 6-9 January 1992, Reno, USA, AIAA-92-0439.
    • (1992) 30th Aerospace Sciences Meeting & Exhibit
    • Spalart, P.R.1    Allmaras, S.R.2
  • 10
    • 84872773746 scopus 로고    scopus 로고
    • Study of supersonic flow separation induced by side jets and its control
    • accepted for publication New Results in Numerical and Experimental Fluid Mechanics V, 14th STAB/DGLR Symposium Bremen, ZARM, Germany 2004
    • KOVAR, A. and SCHÜLEIN, E. Study of supersonic flow separation induced by side jets and its control, accepted for publication in Notes on Numerical Fluid Mechanics and Multisidisciplinary Design - New Results in Numerical and Experimental Fluid Mechanics V, 2006, 14th STAB/DGLR Symposium Bremen, ZARM, Germany 2004.
    • (2006) Notes on Numerical Fluid Mechanics and Multisidisciplinary Design
    • Kovar, A.1    Schülein, E.2
  • 11
    • 0041708667 scopus 로고
    • Aerodynamic interaction effects ahead of rectangular sonic jets exhausting perpendicularly from a flat plate into a Mach number 6 Free Stream
    • National Aeronautics and Space Administration (NASA), Washington, USA
    • ROMEO, D.J. Aerodynamic interaction effects ahead of rectangular sonic jets exhausting perpendicularly from a flat plate into a Mach number 6 Free Stream, Technical Note D-1800, 1963, National Aeronautics and Space Administration (NASA), Washington, USA.
    • (1963) Technical Note , vol.D-1800
    • Romeo, D.J.1
  • 12
    • 0038596508 scopus 로고
    • Three-dimensional effects in shock-seperated flow Regions ahead of lateral control-jets issuing from slot nozzles of finite length
    • AGARD-CP-4, Part 2
    • MAURER, F. Three-dimensional effects in shock-seperated flow Regions ahead of lateral control-jets issuing from slot nozzles of finite length, AGARD-CP-4, Part 2, Flow Separation, 1966, pp 605-634
    • (1966) Flow Separation , pp. 605-634
    • Maurer, F.1
  • 14
    • 0015068831 scopus 로고
    • Multiple jets exhausting into a cross flow
    • ZIEGLER, H. and WOOLER, P.T. Multiple jets exhausting into a cross flow, J Aircr, 1971, 8, (6).
    • (1971) J Aircr , vol.8 , Issue.6
    • Ziegler, H.1    Wooler, P.T.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.