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Volumn , Issue , 2008, Pages

PSP and PIV investigations on the VFE-2 configuration in sub- and transonic flow

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; DELTA WING AIRCRAFT; PAINT; REYNOLDS NUMBER; SHOCK WAVES; VELOCITY MEASUREMENT; WINGS;

EID: 78149440356     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-379     Document Type: Conference Paper
Times cited : (36)

References (28)
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  • 11
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    • Leading edge vortex flow computations and comparison with DNW-HST wind tunnel data
    • Loen, Norway, 7-11 May, Meeting Proceedings RTO-MP-069 (I), SYA 14-1 to 14-13, 2003
    • Brandsma, F.J., Kok, J.C., Dol, H.S., and Elsenaar, A., "Leading edge vortex flow computations and comparison with DNW-HST wind tunnel data, " RTO AVT Symposium on Vortex Flow and High Angle of Attack Aerodynamics, Loen, Norway, 7-11 May 2001, Meeting Proceedings RTO-MP-069 (I), SYA 14-1 to 14-13, 2003.
    • (2001) RTO AVT Symposium on Vortex Flow and High Angle of Attack Aerodynamics
    • Brandsma, F.J.1    Kok, J.C.2    Dol, H.S.3    Elsenaar, A.4
  • 12
    • 0037812306 scopus 로고    scopus 로고
    • Detached-eddy simulations and Reynolds-averaged Navier-stokes simulations of delta wing vortical flowfields
    • AIAA Paper 2002-0587, and, 2002
    • Morton, S.A., Forsythe, J.R., Mitchell, A.M., and Hajek, D., "Detached-eddy simulations and Reynolds-averaged Navier-Stokes simulations of delta wing vortical flowfields, " AIAA Paper 2002-0587, 2002, and J. Fluids Eng. Vol. 124, No. 4,, pp. 924 - 932, 2002.
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  • 13
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    • A new vortex flow experiment for computer code validation
    • Loen, Norway, 7-11 May, Meeting Proceedings RTO-MP-069 (I), SYA 8-1 to 8-31, 2003
    • Hummel, D., and Redeker, G., "A new vortex flow experiment for computer code validation, " RTO AVT Symposium on Vortex Flow and High Angle of Attack Aerodynamics, Loen, Norway, 7-11 May 2001, Meeting Proceedings RTO-MP-069 (I), SYA 8-1 to 8-31, 2003.
    • (2001) RTO AVT Symposium on Vortex Flow and High Angle of Attack Aerodynamics
    • Hummel, D.1    Redeker, G.2
  • 17
    • 39149136190 scopus 로고    scopus 로고
    • Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing
    • DOI 10.1007/s00348-007-0445-5
    • Konrath, R., Klein, C., Schröder, A., Kompenhans, J., "Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing", Experiments in Fluids, DOI 10.1007/s00348-007- 0445-5, 2007.
    • (2007) Experiments in Fluids
    • Konrath, R.1    Klein, C.2    Schröder, A.3    Kompenhans, J.4
  • 21
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    • Application of pressure-sensitive paint for determination of the pressure field and calculation of the forces and moments of models in a wind tunnel
    • Klein, C., Engler, R.H., Henne, U., Sachs, W., "Application of pressure-sensitive paint for determination of the pressure field and calculation of the forces and moments of models in a wind tunnel", Experiments in Fluids 39: 475-483, 2005.
    • (2005) Experiments in Fluids , vol.39 , pp. 475-483
    • Klein, C.1    Engler, R.H.2    Henne, U.3    Sachs, W.4
  • 22
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    • Grant, Ian [Hrsg.]:, CD ROM Proceedings (Session12-5), Optimage Ltd. Edinburgh, UK, S. 1 - 12, Göttingen, Germany, 10.09.-14.09. ISBN 0-9533991-8-4
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  • 26
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.