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Volumn 30, Issue 6, 1993, Pages 689-695

Unsteady flow separation on slender bodies at high angles of attack

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CONTROL SYSTEMS; FLUID MECHANICS; MISSILES;

EID: 0027695723     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.26374     Document Type: Article
Times cited : (16)

References (16)
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  • 3
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  • 4
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    • Aerodynamic Aspects of Aircraft Dynamics at High Angles of Attack
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    • Orlik-Ruckemann, K.J.1
  • 5
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    • Orlik-Ruckemann, K. J., “Aerodynamic Coupling Between Lateral and Longitudinal Degrees of Freedom,” AIAA Journal, Vol. 15, No. 12, 1977, pp. 1792-1799.
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    • Orlik-Ruckemann, K.J.1
  • 6
    • 0038535441 scopus 로고
    • Asymmetric Vortex Shedding from Bodies of Revolution
    • edited by M. J. Heihsch and J. N. Nielsen, Progress in Astronautics and Aeronautics, AIAA, New York, Chap. VII
    • Ericsson, L. E., and Reding, J. P., “Asymmetric Vortex Shedding from Bodies of Revolution,” Tactical Missile Aerodynamics, edited by M. J. Heihsch and J. N. Nielsen, Vol. 104, Progress in Astronautics and Aeronautics, AIAA, New York, 1986, Chap. VII, pp. 243-296.
    • (1986) Tactical Missile Aerodynamics , vol.104 , pp. 243-296
    • Ericsson, L.E.1    Reding, J.P.2
  • 7
    • 0024606452 scopus 로고
    • Wing Rock Generated by Forebody Vortices
    • Ericsson, L. E., “Wing Rock Generated by Forebody Vortices,” Journal of Aircraft, Vol. 26, No. 2, 1989, pp. 110-116.
    • (1989) Journal of Aircraft , vol.26 , Issue.2 , pp. 110-116
    • Ericsson, L.E.1
  • 8
    • 0024104008 scopus 로고
    • Moving Wall Effects in Unsteady Flow
    • Ericsson, L. E., “Moving Wall Effects in Unsteady Flow,” Journal of Aircraft, Vol. 25, No. 11, 1988, pp. 977-990.
    • (1988) Journal of Aircraft , vol.25 , Issue.11 , pp. 977-990
    • Ericsson, L.E.1
  • 9
    • 84975691472 scopus 로고
    • The Scaling and Control of Vortex Geometry Behind Pitching Cylinders
    • Montevidas, R. E., Reisenthel, P., and Nagib, H. N., “The Scaling and Control of Vortex Geometry Behind Pitching Cylinders,” AIAA Paper 89-1003, March 1989.
    • (1989) AIAA Paper 89-1003
    • Montevidas, R.E.1    Reisenthel, P.2    Nagib, H.N.3
  • 10
    • 3743049898 scopus 로고
    • Effects of Mach Number and Afterbody Length on Onset of Asymmetric Forces on Bodies at Zero Sideslip and High Angles of Attack
    • Keener, E. R., Chapman, G. T., and Kruse, R. L., “Effects of Mach Number and Afterbody Length on Onset of Asymmetric Forces on Bodies at Zero Sideslip and High Angles of Attack,” AIAA Paper 76-66, Jan 1976.
    • (1976) AIAA Paper 76-66
    • Keener, E.R.1    Chapman, G.T.2    Kruse, R.L.3
  • 11
    • 85002688343 scopus 로고
    • Über Wirbelsysteme an schlanken Rotationskörpern und ihren Einfluss auf die aerodynamische Beiwerte
    • Saint Louis, France
    • Fiechter, M., “Über Wirbelsysteme an schlanken Rotationskörpern und ihren Einfluss auf die aerodynamische Beiwerte,” Bericht 10/66, Deutsch-Französisches Forchungsinstitut, Saint Louis, France, Dec 1966.
    • (1966) Bericht 10/66, Deutsch-Französisches Forchungsinstitut
    • Fiechter, M.1
  • 12
    • 5244242471 scopus 로고
    • The Behavior of the Leading-Edge Vortices over a Delta Wing Following a Sudden Change of Incidence
    • England, UK
    • Lambourne, N. C., Bryer, D. W., and Maybrey, J. F. M., “The Behavior of the Leading-Edge Vortices over a Delta Wing Following a Sudden Change of Incidence,” Aeronautical Research Council, R&M 3645, England, UK, March 1969.
    • (1969) Aeronautical Research Council, R&M 3645
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  • 13
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    • Active Control of Asymmetric Vortex Effects
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  • 15
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    • private communication of flow visualization results
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    • (1989)
    • Fidler, J.E.1
  • 16
    • 0025480745 scopus 로고
    • Lateral Oscillations of Sting-Mounted Models at High Alpha
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    • Ericsson, L.E.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.