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Volumn , Issue , 2002, Pages

CFD predictions of dynamic derivatives for missiles

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; COMPUTATIONAL FLUID DYNAMICS; DAMPING; MISSILES; ROLLS (MACHINE COMPONENTS);

EID: 85087605143     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-276     Document Type: Conference Paper
Times cited : (60)

References (22)
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  • 3
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    • Oberkamph, W.O.1
  • 5
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    • Mikhail, A.G.1
  • 6
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    • (1994) USER3D, 3-Dimensional Unstructured Euler Solver
    • Oktay, E.1
  • 9
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    • Oktay, E.1    Asma, C.O.2
  • 10
    • 0026367896 scopus 로고
    • A Finite Volume Method for the Euler Equations on Arbitrary Lagrangian-Eulerian Grids
    • Trepanier, J.Y., Reggio, M, Zhang, H, Camarero, R., "A Finite Volume Method for the Euler Equations on Arbitrary Lagrangian-Eulerian Grids, " Computers and Fluids, Vol.20, No.4, 1991, pp. 399-409.
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  • 12
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    • (2000) Proceedings of Parallel CFD '99 , pp. 415-422
    • Uzun, A.1    Akay, H.U.2    Bronnenberg, C.3
  • 14
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  • 17
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  • 18
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    • Batina, J.T.1
  • 19
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  • 20
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.