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Volumn , Issue , 1997, Pages

Calculation of pitch damping coefficients for projectiles

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYERS; DAMPING; FLOW SEPARATION; HYPERSONIC BOUNDARY LAYERS; NUMERICAL METHODS; PROJECTILES; SHOCK WAVES; TURBULENCE MODELS; VISCOUS FLOW;

EID: 84983159794     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (19)
  • 1
    • 0003742644 scopus 로고
    • U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground, Maryland, Report № 1216, My
    • Murphy, C.H. "Free flight motion of symmetric missiles", U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground, Maryland, Report № 1216, My 1963.
    • (1963) Free flight motion of symmetric missiles
    • Murphy, C.H.1
  • 2
    • 85007668755 scopus 로고
    • Aerodynamics of bodies of revolution in coning motion
    • January
    • Tobak, M., Schiff, L.B. and Peterson, V.L. "Aerodynamics of bodies of revolution in coning motion", AIAA I, Vol. 7, № 1, January 1969, pp95-9.
    • (1969) AIAA I , vol.7 , Issue.1 , pp. 95-99
    • Tobak, M.1    Schiff, L.B.2    Peterson, V.L.3
  • 3
    • 0014871899 scopus 로고
    • Results from a new wind-tunnel apparatus for studying coning and spinning motions of bodies of revolution
    • November
    • Schiff, L.B. and Tobak, M. "Results from a new wind-tunnel apparatus for studying coning and spinning motions of bodies of revolution", AIAA J. Vol.8, № 11, November 1970, pp. 1953-1957.
    • (1970) AIAA J , vol.8 , Issue.11 , pp. 1953-1957
    • Schiff, L.B.1    Tobak, M.2
  • 5
    • 0015434616 scopus 로고
    • Nonlinear aerodynamics of bodies in coning motion
    • November
    • Schiff, L.B. "Nonlinear aerodynamics of bodies in coning motion", AIAA J. Vol.10, № 11, November 1972, pp. 1517-1522.
    • (1972) AIAA J , vol.10 , Issue.11 , pp. 1517-1522
    • Schiff, L.B.1
  • 12
    • 33751417048 scopus 로고
    • Finite volume 3DNS and PNS solutions of hypersonic viscous flows around a delta wing using Osher’s flux-difference splitting
    • Qin, N. and Richards, B.E. "Finite volume 3DNS and PNS solutions of hypersonic viscous flows around a delta wing using Osher’s flux-difference splitting", Proceedings of Workshop on Hypersonic Flows for Re-entry Problems, Vol.2, 1990, pp. 947-959.
    • (1990) Proceedings of Workshop on Hypersonic Flows for Re-entry Problems , vol.2 , pp. 947-959
    • Qin, N.1    Richards, B.E.2
  • 15
    • 84968510942 scopus 로고
    • Upwind difference schemes for hyperbolic systems of conservation laws
    • Osher, S. and Solomon, F. "Upwind difference schemes for hyperbolic systems of conservation laws", Mathematics of computation, Vol. 38, № 158, 1982.
    • (1982) Mathematics of computation , vol.38 , Issue.158
    • Osher, S.1    Solomon, F.2
  • 17
    • 0001683376 scopus 로고
    • Computation of turbulent supersonic flows around bodies having cross-flow separation
    • Degani, D. and Schiff, B., "Computation of turbulent supersonic flows around bodies having cross-flow separation", J. Comp. Physics, Vol. 66, № 1, 1986, pp. 173-96.
    • (1986) J. Comp. Physics , vol.66 , Issue.1 , pp. 173-196
    • Degani, D.1    Schiff, B.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.