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Volumn 33, Issue 3, 1996, Pages 477-484

Difficulties in predicting vortex breakdown effects on a rolling delta wing

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DELTA WING AIRCRAFT; FORECASTING; NUMERICAL METHODS; OSCILLATIONS; UNSTEADY FLOW; VORTEX FLOW;

EID: 0030141271     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46969     Document Type: Article
Times cited : (14)

References (29)
  • 3
    • 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
  • 4
    • 0028542221 scopus 로고
    • Further Analysis of High-Rate Rolling Experiments of a 65-Deg Delta Wing
    • Ericsson, L. E., and Hanff, E. S., "Further Analysis of High-Rate 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
  • 6
    • 0006571210 scopus 로고
    • Flow Physics of Critical States for Rolling Delta Wings
    • Ericsson, L. E., "Flow Physics of Critical States for Rolling Delta Wings," Journal of Aircraft, Vol. 32, No. 3, 1995, pp. 603-610.
    • (1995) Journal of Aircraft , vol.32 , Issue.3 , pp. 603-610
    • Ericsson, L.E.1
  • 7
    • 0026685438 scopus 로고
    • Agility as a Contributor to Design Balance
    • Skow, A. M., "Agility as a Contributor to Design Balance," Journal of Aircraft, Vol. 29, No. 1, 1992, pp. 34-46.
    • (1992) Journal of Aircraft , vol.29 , Issue.1 , pp. 34-46
    • Skow, A.M.1
  • 10
    • 0015021235 scopus 로고
    • Vortex Breakdown on Slender Sharp-Edged Delta Wings
    • Wentz, W. H., and Kohlman, D. L., "Vortex Breakdown on Slender Sharp-Edged Delta 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
  • 13
    • 0022915693 scopus 로고
    • Dynamic Support Interference in High-Alpha Testing
    • Ericsson, L. E., and Reding, J. P., "Dynamic Support Interference in High-Alpha Testing," Journal of Aircraft, Vol. 23, No. 12, 1986, pp. 889-896.
    • (1986) Journal of Aircraft , vol.23 , Issue.12 , pp. 889-896
    • Ericsson, L.E.1    Reding, J.P.2
  • 14
    • 0026221405 scopus 로고
    • Another Look at High-Alpha Support Interference
    • Ericsson, L. E., "Another Look at High-Alpha Support Interference," Journal of Aircraft, Vol. 28, No. 5, 1991, pp. 584-591.
    • (1991) Journal of Aircraft , vol.28 , Issue.5 , pp. 584-591
    • Ericsson, L.E.1
  • 15
    • 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
  • 16
    • 0023089232 scopus 로고
    • Reflections Regarding Recent Rotary Rig Results
    • Ericsson, L. E., "Reflections Regarding Recent Rotary Rig Results," Journal of Aircraft, Vol. 24, No. 1, 1987, pp. 25-30.
    • (1987) Journal of Aircraft , vol.24 , Issue.1 , pp. 25-30
    • Ericsson, L.E.1
  • 17
    • 0025682191 scopus 로고
    • Effects of Transition on Wind Tunnel Simulation of Vehicle Dynamics
    • Ericsson, L. E., "Effects of Transition on Wind Tunnel Simulation of Vehicle Dynamics," Progress in Aerospace Sciences, Vol. 27, 1990, pp. 121-144.
    • (1990) Progress in Aerospace Sciences , vol.27 , pp. 121-144
    • Ericsson, L.E.1
  • 18
    • 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
  • 19
    • 0029343499 scopus 로고
    • Vortex Breakdown Control by Delta Wing Geometry
    • Lowson, M. V., and Rily, A. J., "Vortex Breakdown Control by Delta Wing Geometry," Journal of Aircraft, Vol. 32, No. 4, 1995, pp. 832-838.
    • (1995) Journal of Aircraft , vol.32 , Issue.4 , pp. 832-838
    • Lowson, M.V.1    Rily, A.J.2
  • 23
    • 0027623710 scopus 로고
    • Control of Vortices on a Delta Wing by Leading-Edge Injection
    • Gu, W., Robinson, O., and Rockwell, D., "Control of Vortices on a Delta Wing by Leading-Edge Injection," AIAA Journal, Vol. 31, No. 7, 1993, pp. 1177-1186.
    • (1993) AIAA Journal , vol.31 , Issue.7 , pp. 1177-1186
    • Gu, W.1    Robinson, O.2    Rockwell, D.3
  • 25
    • 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 in Aerospace Sciences, Vol. 24, 1987, pp. 249-356.
    • (1987) Progress in Aerospace Sciences , vol.24 , pp. 249-356
    • Ericsson, L.E.1    Reding, J.P.2
  • 26
    • 0026715408 scopus 로고
    • Rapid Prediction of High-Alpha Unsteady Aerodynamics of Slender-Wing Aircraft
    • Ericsson, L. E., and King, H. H. C., "Rapid Prediction of High-Alpha Unsteady Aerodynamics of Slender-Wing Aircraft," Journal of Aircraft, Vol. 29, No. 1, 1992, pp. 85-92.
    • (1992) Journal of Aircraft , vol.29 , Issue.1 , pp. 85-92
    • Ericsson, L.E.1    King, H.H.C.2
  • 28
    • 85033865619 scopus 로고
    • private communication, Nov.
    • Tobak, M., private communication, Nov. 1995.
    • (1995)
    • Tobak, M.1
  • 29
    • 85033851513 scopus 로고
    • private communication, Oct.
    • Huang, X. Z., private communication, Oct. 1995.
    • (1995)
    • Huang, X.Z.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.