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Volumn 100, Issue 997, 1996, Pages 297-303

Structural dynamics-CFD interaction for computation of vertical tail buffet

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; BENDING (DEFORMATION); CALCULATIONS; COMPUTATIONAL FLUID DYNAMICS; DEFLECTION (STRUCTURES); DYNAMICS; NAVIER STOKES EQUATIONS; OSCILLATIONS; REYNOLDS NUMBER; TORSIONAL STRESS; VORTEX FLOW; WINGS;

EID: 0030217458     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article
Times cited : (16)

References (18)
  • 3
    • 2342613428 scopus 로고
    • Vortex-fin interaction on a fighter aircraft
    • AIAA paper 87-2474, Monterey, CA August
    • WENTZ, W.H. Vortex-fin interaction on a fighter aircraft, AIAA paper 87-2474, AIAA Fifth Applied Aerodynamics Conference, Monterey, CA August 1987.
    • (1987) AIAA Fifth Applied Aerodynamics Conference
    • Wentz, W.H.1
  • 9
    • 85001948908 scopus 로고
    • Simulation of tail buffet using delta wing-vertical tail configuration
    • AIAA paper 93-3688-CP, Momerery, CA, August
    • KANDIL, O.A., KANDIL, H.A. and MASSEY, S.J. Simulation of tail buffet using delta wing-vertical tail configuration, AIAA paper 93-3688-CP, AIAA Atmospheric Flight Mechanics Conference, Momerery, CA, August 1993, pp 566-577.
    • (1993) AIAA Atmospheric Flight Mechanics Conference , pp. 566-577
    • Kandil, O.A.1    Kandil, H.A.2    Massey, S.J.3
  • 12
    • 0028699267 scopus 로고
    • Computations of vortex-breakdown induced tail buffet undergoing bending and torsional vibrations
    • AIAA paper 94-1428-CP, AIAA/ASME/ASCE/ASC Structural, SC April
    • KANDIL, O.A., MASSEY, S.J. and KANDIL, H.A. Computations of vortex-breakdown induced tail buffet undergoing bending and torsional vibrations, AIAA paper 94-1428-CP, AIAA/ASME/ASCE/ASC Structural, Structural Dynamics and Material Conference, SC April 1994, pp 977-993.
    • (1994) Structural Dynamics and Material Conference , pp. 977-993
    • Kandil, O.A.1    Massey, S.J.2    Kandil, H.A.3
  • 13
    • 0008426155 scopus 로고    scopus 로고
    • Twin tail/delta wing configuration buffet due to unsteady vortex breakdown flow
    • AIAA paper 96-2517-CP, 17-20 June
    • KANDIL, O.A., SHETA, E.F. and MASSEY, S.J. Twin tail/delta wing configuration buffet due to unsteady vortex breakdown flow, AIAA paper 96-2517-CP, 14th AIAA Applied Aerodynamics Conference, 17-20 June 1996, Vol 2, pp 1136-1150.
    • (1996) 14th AIAA Applied Aerodynamics Conference , vol.2 , pp. 1136-1150
    • Kandil, O.A.1    Sheta, E.F.2    Massey, S.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.