메뉴 건너뛰기




Volumn 51, Issue 2, 2014, Pages 468-477

Two-dimensional potential method simulations of a body-strake configuration

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; BOUNDARY LAYERS; FLOW FIELDS; VORTEX FLOW;

EID: 84898420316     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.A32565     Document Type: Article
Times cited : (3)

References (30)
  • 1
    • 0011303009 scopus 로고
    • Equivalent angle-of-attack concept
    • AIAA, New York
    • Hemsch, M. J., and Nielsen, J. N., "Equivalent Angle-of-Attack Concept," Tactical Missile Aerodynamics, AIAA, New York, 1986, pp. 482-518.
    • (1986) Tactical Missile Aerodynamics , pp. 482-518
    • Hemsch, M.J.1    Nielsen, J.N.2
  • 4
    • 85024590438 scopus 로고
    • Symmetric vortex separation on circular cylinders and cones
    • Dec. doi:10.1115/1.3644003
    • Bryson, A. E., "Symmetric Vortex Separation on Circular Cylinders and Cones," Journal of Applied Mechanics, Vol. 26, No. 4, Dec. 1959, pp. 643-648. doi:10.1115/1.3644003
    • (1959) Journal of Applied Mechanics , vol.26 , Issue.4 , pp. 643-648
    • Bryson, A.E.1
  • 5
    • 0002297003 scopus 로고
    • Ecoulement au Voisinage de la Ponte Avant d'Une Aile a Forte Fleche aux Incidences Moyennes
    • Nov.-Dec.
    • Legendre, R., "Ecoulement au Voisinage de la Ponte Avant d'Une Aile a Forte Fleche aux Incidences Moyennes," La Recherche Aeronautique Bulletin Bimestriel, No. 30, Nov.-Dec. 1952.
    • (1952) La Recherche Aeronautique Bulletin Bimestriel , vol.30
    • Legendre, R.1
  • 6
    • 0013059894 scopus 로고
    • Leading-edge separation from delta wings at supersonic speeds
    • June doi:10.2514/8.2663
    • Adams, M. C., "Leading-Edge Separation from Delta Wings at Supersonic Speeds," Journal of the Aeronautical Sciences, Vol. 20, No. 6, June 1953, p. 430. doi:10.2514/8.2663
    • (1953) Journal of the Aeronautical Sciences , vol.20 , Issue.6 , pp. 430
    • Adams, M.C.1
  • 10
    • 84880920337 scopus 로고
    • An inviscid model of two-dimensional vortex shedding for transient and asymptotically steady separated flow over a cylinder
    • Jan.
    • Sarpkaya, T., and Shoaff, R., "An Inviscid Model of Two-Dimensional Vortex Shedding for Transient and Asymptotically Steady Separated Flow over a Cylinder," 17th Aerospace Sciences Meeting, AIAA Paper 1979-0281, Jan. 1979.
    • (1979) 17th Aerospace Sciences Meeting, AIAA Paper 1979-0281
    • Sarpkaya, T.1    Shoaff, R.2
  • 13
    • 0015201501 scopus 로고
    • A multi-vortex method for axisymmetric bodies at angle of attack
    • Dec. doi:10.2514/3.44317
    • Angelucci, S. B. A., "A Multi-Vortex Method for Axisymmetric Bodies at Angle of Attack," Journal of Aircraft, Vol. 8, No. 12, Dec. 1971, pp. 959-966. doi:10.2514/3.44317
    • (1971) Journal of Aircraft , vol.8 , Issue.12 , pp. 959-966
    • Angelucci, S.B.A.1
  • 15
    • 85084012104 scopus 로고
    • Multivortex model of asymmetric shedding on slender bodies at high angle of attack
    • Jan.
    • Wardlaw, A. B., "Multivortex Model of Asymmetric Shedding on Slender Bodies at High Angle of Attack," 13th Aerospace Sciences Meeting, AIAA Paper 1975-0123, Jan. 1975.
    • (1975) 13th Aerospace Sciences Meeting, AIAA Paper 1975-0123
    • Wardlaw, A.B.1
  • 21
    • 84880924675 scopus 로고    scopus 로고
    • Lee side flow structures of very low aspect ratio cruciform wing-body configurations
    • Tuling, S., Dala, L., and Toomer, C., "Lee Side Flow Structures of Very Low Aspect Ratio Cruciform Wing-Body Configurations," Journal of Spacecraft and Rockets, Vol. 50, No. 6, 2013, pp. 1134-1149.
    • (2013) Journal of Spacecraft and Rockets , vol.50 , Issue.6 , pp. 1134-1149
    • Tuling, S.1    Dala, L.2    Toomer, C.3
  • 26
    • 0004196981 scopus 로고
    • Nielsen Engineering and Research, Inc., Mountainview, CA
    • Nielsen, J. N., "Missile Aerodynamics," Nielsen Engineering and Research, Inc., Mountainview, CA, 1988.
    • (1988) Missile Aerodynamics
    • Nielsen, J.N.1
  • 29
    • 84958430400 scopus 로고
    • The prediction of separation of the turbulent boundary layer
    • July, doi:10.1017/S0022112059000015
    • Stratford, B.S., "The Prediction of Separation of the Turbulent Boundary Layer," Journal of Fluid Mechanics, Vol. 5, No. 1, July 1958, pp. 1-16. doi:10.1017/S0022112059000015
    • (1958) Journal of Fluid Mechanics , vol.5 , Issue.1 , pp. 1-16
    • Stratford, B.S.1
  • 30
    • 84880916424 scopus 로고    scopus 로고
    • Some compressibility effects on the lee side flow structures of cruciform wing-body configurations with very low aspect ratio wings
    • Aug. doi:10.1016/j.ast.2013.04.008
    • Tuling, S., Dala, L., and Toomer, C., "Some Compressibility Effects on the Lee Side Flow Structures of Cruciform Wing-Body Configurations with Very Low Aspect Ratio Wings," Aerospace Science and Technology, Vol. 29, No. 1, Aug. 2013, pp. 373-385. doi:10.1016/j.ast.2013.04.008
    • (2013) Aerospace Science and Technology , vol.29 , Issue.1 , pp. 373-385
    • Tuling, S.1    Dala, L.2    Toomer, C.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.