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Volumn 31, Issue 6, 1994, Pages 1350-1357

Further analysis of high-rate rolling experiments of a 65-deg delta wing

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DYNAMICS; FLUID MECHANICS; OSCILLATIONS; VORTEX FLOW;

EID: 0028542221     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.46658     Document Type: Article
Times cited : (34)

References (18)
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    • Skow, A.M.1
  • 3
    • 85003282203 scopus 로고
    • Analysis of wind-tunnel data obtained in high-rate rolling experiments with slender delta wings
    • IAR-CR-14, National Research Council, Ottawa, Canada, Aug
    • Ericsson, L. E., “Analysis of Wind-Tunnel Data Obtained in High-Rate Rolling Experiments with Slender Delta Wings,” Inst, for Aerospace Research, IAR-CR-14, National Research Council, Ottawa, Canada, Aug. 1991.
    • (1991) Inst, for Aerospace Research
    • Ericsson, L.E.1
  • 4
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    • Unique high-alpha roll dynamics of a sharp-edged 65 deg delta wing
    • Ericsson, L. E., and Hanff, E. S., “Unique High-Alpha Roll Dynamics of a Sharp-Edged 65 deg Delta Wing,” Journal of Aircraft, Vol. 31, No. 3, 1994, pp. 520-525.
    • (1994) Journal of Aircraft , vol.31 , Issue.3 , pp. 520-525
    • Ericsson, L.E.1    Hanff, E.S.2
  • 5
    • 0022562096 scopus 로고
    • Fluid dynamics of unsteady separated flow, part i, bodies of revolution
    • Ericsson, L. E., and Reding, J. P., “Fluid Dynamics of Unsteady Separated Flow, Part I, Bodies of Revolution,” Progress of Aerospace Sciences, Vol. 23, 1986, pp. 1-84.
    • (1986) Progress of Aerospace Sciences , vol.23 , pp. 1-84
    • Ericsson, L.E.1    Reding, J.P.2
  • 6
    • 0023589650 scopus 로고
    • Fluid dynamics of unsteady separated flow, part ii, lifting surfaces
    • Ericsson, L. E., and Reding, J. P., “Fluid Dynamics of Unsteady Separated Flow, Part II, Lifting Surfaces,” Progress of Aerospace Sciences, Vol. 24, 1987, pp. 249-356.
    • (1987) Progress of Aerospace Sciences , vol.24 , pp. 249-356
    • Ericsson, L.E.1    Reding, J.P.2
  • 8
    • 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.1    Kohlman, D.L.2
  • 9
    • 0027668701 scopus 로고
    • Effect of leading-edge cross-sectional geometry on slender wing unsteady aerodynamics
    • Ericsson, L. E., and King, H. H. C., “Effect of Leading-Edge Cross-Sectional Geometry on Slender Wing Unsteady Aerodynamics,” Journal of Aircraft, Vol. 30, No. 5, 1993, pp. 793-795.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 793-795
    • Ericsson, L.E.1    King, H.H.C.2
  • 10
    • 0026715408 scopus 로고
    • Rapid prediction of highalpha unsteady aerodynamics of slender-wing aircraft dynamics
    • Ericsson, L. E., and King, H. H. C., “Rapid Prediction of HighAlpha Unsteady Aerodynamics of Slender-Wing Aircraft Dynamics,” Journal of Aircraft, Vol. 29, No. 1, 1992, pp. 85-92.
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    • Ericsson, L.E.1    King, H.H.C.2
  • 11
    • 5244242471 scopus 로고
    • The behavior of the leading edge vortices over a delta wing following a sudden change of incidence
    • R&M 3645, UK, March
    • 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, UK, March 1969.
    • (1969) Aeronautical Research Council
    • Lambourne, N.C.1    Bryer, D.W.2    Maybrey, J.F.M.3
  • 12
    • 0003210574 scopus 로고
    • Fluid mechanics of dynamic stall, part i, unsteady flow concepts
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  • 14
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    • The bursting of leading-edge vortices-some observations and discussion of the phenomenon
    • R&M 3282, UK, April
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  • 15
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    • Ericsson, L.E.1    Reding, J.P.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.