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Volumn 39, Issue 1, 2002, Pages 51-58

Airfoil validation using coupled Navier-Stokes and eN transition prediction methods

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATIONAL METHODS; DRAG; LAMINAR FLOW; LIFT; NAVIER STOKES EQUATIONS; PRESSURE DISTRIBUTION; STABILITY; WIND TUNNELS;

EID: 0036179661     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2894     Document Type: Article
Times cited : (25)

References (21)
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    • Transition, pressure gradient and stability theory
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    • (1956)
    • Smith, A.M.O.1    Gamberoni, N.2
  • 2
    • 0004143477 scopus 로고
    • A suggested semi-emperical method for the calculation of the boundary layer transition region
    • Univ. of Delft, Dept. of Aerospace Engineering, Rept. VTH-74, The Netherlands, Oct.
    • (1956)
    • Van Ingen, J.L.1
  • 7
    • 0032595442 scopus 로고    scopus 로고
    • N transition prediction in Navier-Stokes methods for two dimensional airfoil computations
    • (1999) AIAA Journal , vol.37 , Issue.10 , pp. 1187-1196
    • Stock, H.W.1    Haase, W.2
  • 9
    • 0008426152 scopus 로고
    • Messungen am Laminar-profil DoAL3 im Transsonischen Windkanal Braunschweig (TWB)
    • DLR-Interner Bericht, DLR, German Aerospace Establishment, Rept. IB 129-87/9, Braunschweig, Germany
    • (1987)
    • Müller, R.1    Puffert-Meißner, W.2    Lück, H.3
  • 10
    • 0008444192 scopus 로고
    • Bestimmung des N-Faktors im Transsonischen-Windkanal Braunschweig (TWB) anhand von Druckverteilungs- und Umschlagspunkt messungen und dem Sally-Verfahren
    • edited by Deutsche Gesellschaft für Luft- und Raumfahrt e.V. (DGLR), 8-9.11.1988, DGLR-REP. 88-05, Braunschweig, Germany
    • (1988) 6th DGLR-Fach-Symposium (Strömungen mit Ablösung) , pp. 66-77
    • Köster, H.1    Müller, R.2
  • 11
    • 4243977257 scopus 로고
    • Transition prediction using different linear stability analysis strategies
    • AIAA Paper 94-1848, June
    • (1994)
    • Schrauf, G.1
  • 12
    • 0008507873 scopus 로고
    • Natural laminar flow: A wind tunnel test campaign and comparison with free flight test data
    • AIAA Paper 90-3045, Aug.
    • (1990)
    • Henke, R.1    Münch, F.X.2
  • 16
    • 0008465115 scopus 로고
    • Design and experimental results for a natural-laminar-flow airfoil for general aviation applications
    • NASA TP 1861, April
    • (1981)
    • Somers, D.M.1
  • 17
    • 4244035632 scopus 로고
    • Effects of sweep angle on the boundary-layer stability characteristics of an untapered wing at low speeds
    • NASA TN D-338, Oct.
    • (1960)
    • Boltz, F.W.1    Kenyon, G.C.2    Allen, C.Q.3
  • 19
    • 0022162768 scopus 로고
    • A mathematical simple turbulence closure model for attached and separated turbulent boundary layers
    • (1985) AIAA Journal , vol.23 , Issue.11 , pp. 1684-1692
    • Johnson, D.A.1    King, L.S.2
  • 21
    • 0008461889 scopus 로고
    • An efficient solver of the eigenvalue problem of the linear-stability equations for three-dimensional, compressible boundary layer flows
    • edited by Deutsche Gesellschaft für Luft, und Raumfahrt e.V. (DGLR), 8-9.11.1988, DGLR-REP. 88-05, Braunschweig, Germany
    • (1988) 6th DGLR-Fach-Symposium (Strömungen mit Ablösung) , pp. 18-27
    • Schrauf, G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.