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Volumn 1, Issue , 2004, Pages 159-177

Vortex flows on a rolling nonslender delta wing

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DELTA WING AIRCRAFT; ELECTRIC MOTORS; FLOW VISUALIZATION; MATHEMATICAL MODELS; REYNOLDS NUMBER; ROLLING; UNMANNED VEHICLES; VELOCITY MEASUREMENT;

EID: 20744437600     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-4729     Document Type: Conference Paper
Times cited : (4)

References (17)
  • 2
    • 0015021235 scopus 로고
    • Vortex breakdown on slender sharp-edged wings
    • Wentz, W. H., and Kohlman, D. L., "Vortex Breakdown on Slender Sharp-Edged Wings," Journal of Aircraft, Vol. 8, No. 3, 1971, pp. 156-161.
    • (1971) Journal of Aircraft , vol.8 , Issue.3 , pp. 156-161
    • Wentz, W.H.A.1    Kohlman, D.L.2
  • 3
    • 0037273369 scopus 로고    scopus 로고
    • Leading-edge vortex structure of nonslender delta wings at low reynolds number
    • Ol, M. V., and Gharib, M., "Leading-Edge Vortex Structure of Nonslender Delta Wings at Low Reynolds Number," AIAA Journal, Vol. 41, No. 1, 2003, pp. 16-26.
    • (2003) AIAA Journal , vol.41 , Issue.1 , pp. 16-26
    • Ol, M.V.A.1    Gharib, M.2
  • 4
    • 0029341383 scopus 로고
    • Flow developments above 50-deg sweep delta wings with different leading-edge profiles
    • Miau, J. J., Kuo, K. T., Liu, W. H., Hsieh, S. J., Chou, J. H., and Lin, C. K., "Flow Developments Above 50-Deg Sweep Delta Wings with Different Leading-Edge Profiles," Journal of Aircraft, Vol. 32, No. 4, 1995, pp. 787-794.
    • (1995) Journal of Aircraft , vol.32 , Issue.4 , pp. 787-794
    • Miau, J.J.1    Kuo, K.T.2    Liu, W.H.3    Hsieh, S.J.4    Chou, J.H.A.5    Lin, C.K.6
  • 5
    • 20744442371 scopus 로고    scopus 로고
    • An experimental investigation of leading edge vortices and passage to stall of nonslender delta wings
    • RTO AVT-072, May Paper 2
    • Ol, M. V., "An Experimental Investigation of Leading Edge Vortices and Passage to Stall of Nonslender Delta Wings," Symposium on Advanced Flow Management, RTO AVT-072, May 2001, Paper 2.
    • (2001) Symposium on Advanced Flow Management
    • Ol, M.V.1
  • 12
    • 0030106742 scopus 로고    scopus 로고
    • Body-axis rolling motion critical states of a 65-degree delta wing
    • Jenkins, J. E., Myatt, J. H., and Hanff, E. S., "Body-Axis Rolling Motion Critical States of a 65-Degree Delta Wing," Journal of Aircraft, Vol. 33, No. 2, 1996, pp. 268-278.
    • (1996) Journal of Aircraft , vol.33 , Issue.2 , pp. 268-278
    • Jenkins, J.E.1    Myatt, J.H.A.2    Hanff, E.S.3
  • 15
    • 0029378755 scopus 로고
    • Analysis of rolled delta wing flows using effective sweep and attack angles
    • Stephen, E. J., "Analysis of Rolled Delta Wing Flows Using Effective Sweep and Attack Angles," Journal of Aircraft, Vol. 32, No. 5, 1995, pp. 978-984.
    • (1995) Journal of Aircraft , vol.32 , Issue.5 , pp. 978-984
    • Stephen, E.J.1
  • 16
    • 0034228182 scopus 로고    scopus 로고
    • Prediction of vortex breakdown location on a banked delta wing
    • Engineering Notes
    • Pelletier, A., and Nelson, R. C., "Prediction of Vortex Breakdown Location on a Banked Delta Wing," Journal of Aircraft, Vol. 37, No. 4, 2000, Engineering Notes.
    • (2000) Journal of Aircraft , vol.37 , Issue.4
    • Pelletier, A.A.1    Nelson, R.C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.