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Volumn 33, Issue 2, 1996, Pages 452-454

Simple prediction method for location of vortex breakdown on delta wings

Author keywords

[No Author keywords available]

Indexed keywords

CORRELATION METHODS; DELTA WING AIRCRAFT; INTERPOLATION; MATHEMATICAL MODELS; VORTEX FLOW;

EID: 0030108128     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46963     Document Type: Article
Times cited : (16)

References (21)
  • 1
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  • 2
    • 84972003628 scopus 로고
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  • 3
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    • Vortex Breakdown on Slender Sharp Edged Wings
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    • (1971) Journal of Aircraft , vol.8 , Issue.3 , pp. 156-161
    • Wentz, W.H.1    Kohlman, D.L.2
  • 4
    • 0029310347 scopus 로고
    • Criteria for Location of Vortex Breakdown over Delta Wings
    • Gursul, I., "Criteria for Location of Vortex Breakdown over Delta Wings," Aeronautical Journal, Vol. 99, No. 985, 1995, pp. 194-196.
    • (1995) Aeronautical Journal , vol.99 , Issue.985 , pp. 194-196
    • Gursul, I.1
  • 5
    • 0027224151 scopus 로고
    • Measurements of Circulation and Vorticity in the Leading-Edge Vortex of a Delta Wing
    • Visser, K. D., and Nelson, R. C., "Measurements of Circulation and Vorticity in the Leading-Edge Vortex of a Delta Wing," AIAA Journal, Vol. 31, No. 1, 1993, pp. 104-111.
    • (1993) AIAA Journal , vol.31 , Issue.1 , pp. 104-111
    • Visser, K.D.1    Nelson, R.C.2
  • 6
    • 0028174512 scopus 로고
    • Simple Numerical Criterion for Vortex Breakdown
    • Robinson, B. A., Barnett, R. M., and Agrawal, S., "Simple Numerical Criterion for Vortex Breakdown," AIAA Journal, Vol. 32, No. 1, 1994, pp. 116-122.
    • (1994) AIAA Journal , vol.32 , Issue.1 , pp. 116-122
    • Robinson, B.A.1    Barnett, R.M.2    Agrawal, S.3
  • 7
    • 0025434835 scopus 로고
    • Connection between Leading Edge Sweep, Vortex Lift, and Vortex Strength for Delta Wings
    • Hemsch, M. J., and Luckring, J. M., "Connection Between Leading Edge Sweep, Vortex Lift, and Vortex Strength for Delta Wings," Journal of Aircraft, Vol. 27, No. 5, 1990, pp. 473-475.
    • (1990) Journal of Aircraft , vol.27 , Issue.5 , pp. 473-475
    • Hemsch, M.J.1    Luckring, J.M.2
  • 12
    • 0020141599 scopus 로고
    • Water-Tunnel Studies of Leading Edge Vortices
    • Erickson, G. E., "Water-Tunnel Studies of Leading Edge Vortices," Journal of Aircraft, Vol. 19, No. 6, 1982, pp. 442-448.
    • (1982) Journal of Aircraft , vol.19 , Issue.6 , pp. 442-448
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  • 13
    • 0025402143 scopus 로고
    • Effects of a Contoured Apex on Vortex Breakdown
    • Panton, R. L., "Effects of a Contoured Apex on Vortex Breakdown," Journal of Aircraft, Vol. 27, No. 3, 1990, pp. 285-288.
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    • Panton, R.L.1
  • 15
    • 0026203428 scopus 로고
    • Separated Flowfield on a Slender Wing Undergoing Transient Pitching Motions
    • Thompson, S. A., Batill, S. M., and Nelson, R. C., "Separated Flowfield on a Slender Wing Undergoing Transient Pitching Motions," Journal of Aircraft, Vol. 28, No. 8, 1991, pp. 489-495.
    • (1991) Journal of Aircraft , vol.28 , Issue.8 , pp. 489-495
    • Thompson, S.A.1    Batill, S.M.2    Nelson, R.C.3
  • 19
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    • Visualization and Wake Surveys of Vortical Flow over a Delta Wing
    • Payne, F. M., Ng, T. T., Nelson, R. C., and Schiff, L. B., "Visualization and Wake Surveys of Vortical Flow over a Delta Wing," AIAA Journal, Vol. 26, No. 1, 1988, pp. 137-143.
    • (1988) AIAA Journal , vol.26 , Issue.1 , pp. 137-143
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  • 20
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    • (1978) Dynamic Stability Parameter
    • Skow, A.M.1    Titiriga, A.2
  • 21
    • 0003328032 scopus 로고
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    • Jan.-Feb.
    • Werle, H., "Sur l'eclatement des Tourbillons d'apex d'une Aile Delta aux Fibles Vitesses," La Recherche Aeronautique, Vol. 74, Jan.-Feb. 1960, pp. 23-30.
    • (1960) La Recherche Aeronautique , vol.74 , pp. 23-30
    • Werle, H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.