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Volumn 32, Issue 3, 1995, Pages 603-610

Flow physics of critical states for rolling delta wings

(1)  Ericsson, Lars E a  

a NONE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

VORTEX FLOW; WINGS;

EID: 0006571210     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.46762     Document Type: Article
Times cited : (29)

References (21)
  • 4
    • 0028424899 scopus 로고
    • 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
    • 0028542221 scopus 로고
    • Further Analysis of HighRate Rolling Experiments of a 65 Deg Delta Wing
    • Ericsson, L. E., and Hanff, E. S., “Further Analysis of HighRate Rolling Experiments of a 65 Deg Delta Wing,” Journal of Aircraft, Vol. 31, No. 6, 1994, pp. 1350-1357.
    • (1994) Journal of Aircraft , vol.31 , Issue.6 , pp. 1350-1357
    • Ericsson, L.E.1    Hanff, E.S.2
  • 7
    • 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
  • 8
    • 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
  • 9
    • 22844440260 scopus 로고
    • Vortex Breakdown Control by Delta Wing Geometry
    • Lowson, M. V., and Rily, A. J., “Vortex Breakdown Control by Delta Wing Geometry,” AIAA Paper 94-3487, Aug. 1994.
    • (1994) AIAA Paper , pp. 94-3487
    • Lowson, M.V.1    Rily, A.J.2
  • 10
  • 11
    • 85003220382 scopus 로고
    • Aeroelastic Instability Caused by Slender Payloads
    • Ericsson, L. E., “Aeroelastic Instability Caused by Slender Payloads,” Journal of Spacecraft and Rockets, Vol. 4, No. 1, 1967, pp. 65-73.
    • (1967) Journal of Spacecraft and Rockets , vol.4 , Issue.1 , pp. 65-73
    • Ericsson, L.E.1
  • 12
    • 0343478562 scopus 로고
    • Unsteady Pressure Phenomena for Basic Missile Shapes at Transonic Speeds
    • Robertson, J. E., “Unsteady Pressure Phenomena for Basic Missile Shapes at Transonic Speeds,” AIAA Paper 64-3, Jan. 1963.
    • (1963) AIAA Paper , pp. 64-73
    • Robertson, J.E.1
  • 13
    • 84910584744 scopus 로고
    • Characteristics of Steady State Pressures on the Cylindrical Portion of Cone-Cylinder Bodies at Transonic Speeds, Arnold Engineering Development Center
    • Robertson, J. E., and Chevalier, H. L., “Characteristics of Steady State Pressures on the Cylindrical Portion of Cone-Cylinder Bodies at Transonic Speeds,” Arnold Engineering Development Center, TDR-63-104, Aug. 1963.
    • (1963) TDR , pp. 63-104
    • Robertson, J.E.1    Chevalier, H.2
  • 14
    • 85003415015 scopus 로고
    • Pressure Fluctuations Resulting from Alternating Flow Separation and Attachment at Transonic Speeds, Arnold Engineering Development Center
    • Chevalier, H. L., and Robertson, J. E., “Pressure Fluctuations Resulting from Alternating Flow Separation and Attachment at Transonic Speeds,” Arnold Engineering Development Center, TDR-63-204, Nov. 1963.
    • (1963) TDR-63 , pp. 204
    • Chevalier, H.L.1    Robertson, J.2
  • 15
  • 17
    • 0003210574 scopus 로고
    • Fluid Mechanics of Dynamic Stall, Part I, Unsteady Flow Concepts
    • Ericsson, L. E., and Reding, J. P., “Fluid Mechanics of Dynamic Stall, Part I, Unsteady Flow Concepts,” Journal of Fluids and Structures, Vol. 2, No. 1, 1988, pp. 1-33.
    • (1988) Journal of Fluids and Structures , vol.2 , Issue.1 , pp. 1-33
    • Ericsson, L.E.1    Reding, J.P.2
  • 18
    • 0003339875 scopus 로고
    • Prediction of Leading-Edge Vortex Breakdown on a Delta Wing Oscillating in Roll
    • Huang, X. Z., and Hanff, E. S., “Prediction of Leading-Edge Vortex Breakdown on a Delta Wing Oscillating in Roll,” AIAA Paper 92-2677, June 1992.
    • (1992) AIAA Paper , pp. 92-2677
    • Huang, X.Z.1    Hanff, E.S.2
  • 19
    • 0027667663 scopus 로고
    • Ground Facility Interference on Aircraft Configurations with Separated Flow
    • Beyers, M. E., and Ericsson, L. E., “Ground Facility Interference on Aircraft Configurations with Separated Flow,” Journal of Aircraft, Vol. 30, No. 5, 1993, pp. 682-688.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 682-688
    • Beyers, M.E.1    Ericsson, L.E.2
  • 21
    • 0026715408 scopus 로고
    • Rapid Prediction of HighAlpha Unsteady Aerodynamics of Slender-Wing Aircraft
    • Ericsson, L. E., and King, H. H. C., “Rapid Prediction of HighAlpha Unsteady Aerodynamics of Slender-Wing Aircraft,” Journal of Aircraft, Vol. 29, No. 1, 1992, p. 85-92.
    • (1992) Journal of Aircraft , vol.29 , Issue.1 , pp. 85-92
    • Ericsson, L.E.1    King, H.H.C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.