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Volumn 2, Issue , 2002, Pages 700-715

Nonlinear aeroelastic computation of wings with pylon/finned-store using parallel unstructured euler solver

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; FINITE ELEMENT METHOD; FLUTTER (AERODYNAMICS); MODAL ANALYSIS; PARALLEL PROCESSING SYSTEMS; SUPERSONIC AERODYNAMICS; TRANSONIC AERODYNAMICS; UNSTEADY FLOW;

EID: 0036079219     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (11)

References (34)
  • 7
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  • 17
    • 0021422150 scopus 로고
    • Wind tunnel correlation study of aerodynamic modeling for F/A-18 wing-store tip-missile flutter
    • May
    • (1984) Journal of Aircraft , vol.21 , Issue.5 , pp. 329-334
    • Triplett, W.E.1
  • 20
    • 0033888852 scopus 로고    scopus 로고
    • Transonic and low-supersonic aerodynamic analysis of a wing with underpylon/store
    • January-February
    • (2000) Journal of Aircraft , vol.37 , Issue.1 , pp. 189-192
    • Kim, D.H.1    Lee, I.2
  • 21
    • 0005812996 scopus 로고    scopus 로고
    • Transonic and supersonic flutter characteristics of a wing-box model with tip stores
    • AIAA Paper , vol.2001 , Issue.1464
    • Kim, D.H.1    Lee, I.2
  • 22
    • 0005856034 scopus 로고    scopus 로고
    • Unsteady flow computations using a 3-D parallel unstructured dynamic mesh adaptation algorithm
    • (2001) AIAA Paper , vol.2001 , Issue.865
    • Park, Y.M.1    Kwon, O.J.2
  • 24
    • 0026617152 scopus 로고
    • Upwind scheme for solving the euler equations on unstructured tetrahedral meshes
    • (1992) AIAA Journal , vol.30 , Issue.1 , pp. 70-77
    • Frink, N.T.1
  • 29
    • 0025475785 scopus 로고
    • Unsteady euler airfoil solutions using unstructured dynamic meshes
    • (1990) AIAA Journal , vol.28 , Issue.8 , pp. 1381-1388
    • Batina, J.T.1
  • 30
    • 0003587244 scopus 로고    scopus 로고
    • An adaptive unstructured grid method by subdivision, local remeshing, and grid movement
    • (1999) AIAA Paper , vol.99 , Issue.3255
    • Pirzadeh, S.Z.1
  • 33
    • 0003345196 scopus 로고
    • AGARD standard aeroelastic configurations for dynamic response. Candidate configuration I: Wing 445.6
    • August
    • (1987) NASA TM 100492
    • Yates E.C., Jr.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.