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Volumn 220, Issue 6, 2006, Pages 559-568

The second international Vortex Flow Experiment (VFE-2): Objectives and first results

Author keywords

CFD; Delta wing; Leading edges rounded; Leading edges sharp; Particle image velocimetry; Pressure sensitive paint

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; HYDRAULIC MODELS; NUMERICAL METHODS; VELOCITY MEASUREMENT; VORTEX FLOW; WIND TUNNELS;

EID: 33947577697     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/09544100JAERO72     Document Type: Article
Times cited : (51)

References (11)
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  • 2
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    • Elsenaar, A., Hjelmberg, L., Bütefisch, K.-A., and Bannink, W. J. The international vortex flow experiment. AGARD-CP 437, 1988, 1, pp. 9-1-9-23.
    • Elsenaar, A., Hjelmberg, L., Bütefisch, K.-A., and Bannink, W. J. The international vortex flow experiment. AGARD-CP 437, 1988, Vol. 1, pp. 9-1-9-23.
  • 3
    • 33947577741 scopus 로고    scopus 로고
    • Wagner, B., Hitzel, S., Schmatz, M. A., Schwarz, W., Hilgenstock, A., and Scherr, S. Status of CFD validation on the vortex flow experiment. AGARD-CP 437, 1988, 1, pp. 10-1-10-10.
    • Wagner, B., Hitzel, S., Schmatz, M. A., Schwarz, W., Hilgenstock, A., and Scherr, S. Status of CFD validation on the vortex flow experiment. AGARD-CP 437, 1988, Vol. 1, pp. 10-1-10-10.
  • 4
    • 78149452571 scopus 로고
    • Modelling and numerical simulation of vortex flow in aerodynamics
    • Hoeijmakers, H. W. M. Modelling and numerical simulation of vortex flow in aerodynamics. AGARD-CP 494, 1991, pp. 1-1-1-46.
    • (1991) AGARD-CP , vol.494
    • Hoeijmakers, H.W.M.1
  • 6
    • 0012314391 scopus 로고    scopus 로고
    • Experimental surface pressure data obtained on 65° delta wing across Reynolds number and Mach number ranges
    • Chu, J. and Luckring, I. M. Experimental surface pressure data obtained on 65° delta wing across Reynolds number and Mach number ranges. NASA TM 4645 (1996).
    • (1996) NASA TM , vol.4645
    • Chu, J.1    Luckring, I.M.2
  • 7
    • 78149428493 scopus 로고    scopus 로고
    • Reynolds number, compressibility, and leading-edge bluntness effects on delta-wing aerodynamics
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    • Luckring, J. M. Reynolds number, compressibility, and leading-edge bluntness effects on delta-wing aerodynamics. ICAS Proceedings, Yokohama, 2004, Paper 4.1.4.
    • (2004) ICAS Proceedings
    • Luckring, J.M.1
  • 8
    • 2642580139 scopus 로고    scopus 로고
    • A review of steps taken to create an international virtual laboratory at NASA Langley for aerodynamic prediction and comparison
    • Lamar, J. E., Cronin, C. K., and Scott, L. E. A review of steps taken to create an international virtual laboratory at NASA Langley for aerodynamic prediction and comparison. Prog. Aerospace Sci., 2004, 40, 163-172.
    • (2004) Prog. Aerospace Sci , vol.40 , pp. 163-172
    • Lamar, J.E.1    Cronin, C.K.2    Scott, L.E.3
  • 11
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    • Experimentelle Untersuchung der Strömung auf der Saugseite eines schlanken Deltaflü gels
    • Hummel, D. Experimentelle Untersuchung der Strömung auf der Saugseite eines schlanken Deltaflü gels. Z. Flugwiss, 1965, 13, 247-252.
    • (1965) Z. Flugwiss , vol.13 , pp. 247-252
    • Hummel, D.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.