Wind tunnel-flight correlation for laminar wings in adiabatic and heating flow conditions

Aerospace Science and Technology

Volumn 6, Issue 4, 2002, Pages 245-257

  Stock, Hans W ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

Adiabatic and heating flow conditions; Entransition prediction; Laminar wing; Navier stokes method

Indexed keywords

COMPUTATIONAL METHODS; CORRELATION METHODS; DRAG; EXTRAPOLATION; FLIGHT DYNAMICS; HEAT TRANSFER; LAMINAR FLOW; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; THERMAL EFFECTS; WIND TUNNELS; WINGS;

ADIABATIC FLIGHT CONDITION; HEATING FLOW CONDITIONS;

AEROSPACE ENGINEERING;

EID: 0036082779     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(02)01166-5     Document Type: Article

References (23)

1. Anon., Two-Dimensional Transonic Testing Methods, Final Report Garteur Action Group AD (AG-02), National Aerospace Laboratory NLR, The Netherlands, 1981, Rept. NLR TR 83086 L.
2. D. Arnal, C. Bulgubure, Drag reduction by boundary-layer laminarisation, La Recherche Aerospatiale, May 1996.
3. D. Arnal, G. Casalis, Laminar-turbulent transition prediction in three-dimensional flows, Progress in Aerospace Sciences 36 (2000) 173-191.
4. W. Haase, EUROVAL - A European initiative on validation of CFD codes, in: Notes on Numerical Fluid Mechanics, Vol. 42, Vieweg Verlag, 1992, pp. 82-87.
5. R. Henke, F.X. Münch, Natural Laminar Flow: A Wind Tunnel Test Campaign and Comparison with Free Flight Test Data, AIAA-90-3045, 1990.
6. K.H. Horstmann, H. Körner, Natural laminar flight test investigation for commuter aircraft application, in: 2nd European Forum on Laminar Flow Technology, 10-12 June, Bordeaux, France, 1996.
7. K.H. Horstmann, R. Müller, P. Dick, W. Wohlrath, Flugversuche am Laminarhandschuh der Do 228, in: 8th DGLR-Fachsymposium Strömung mit Ablösung, 10-12 November, Köln-Porz, DGLR-Bericht 92-07, 1992.
8. K.H. Horstmann, A. Quast, G. Redeker, Flight and wind tunnel investigations on boundary layer transition, Journal of Aircaft 27 (2) (1990) 146-150.
9. K.H. Horstmann, G. Redeker, A. Quast, U. Dressler, H. Bieler, Flight Tests with a Natural Laminar Flow Glove on a Transport Aircraft, AIAA Paper 90-3044, 1990.
10. H.P. Horton, H.W. Stock, Computation of compressible, laminar boundary-layers on swept, tapered wings, Journal of Aircraft 32 (6) (1995) 1402-1405.
11. D.A. Johnson, L.S. King, A mathematical simple turbulence closure model for attached and separated turbulent boundary layers, AIAA Journal 23 (11) (1985) 1684-1692.
12. H. Köster, R. Müller, Bestimmung des N-Faktors im TranssonischenWindkanal Braunschweig (TWB) anhand von Druckverteilungsund Umschlagspunktmessungen und dem Sally-Verfahren, 6th DGLR-Fach-Symposium (Strömungen mit Ablösung), 8-9.11.1988, Braunschweig, DGLR-REP. 88-05, pp. 66-77; Editor: Deutsche Gesellschaft für Luft- und Raumfahrt e.V. (DGLR), Bonn, Germany.
13. R. Müller, W. Puffert-Meißner, H. Lück, Messungen am Laminarprofil DoAL3 im Transsonischen Windkanal Braunschweig (TWB), DLR-Interner Bericht, DLR, German Aerospace Establishment, Braunschweig, Germany, Rept. IB 129-87/9, 1987.
14. G. Schrauf, Linear Stability Theory Applied to Wind Tunnel and Flight Experiments, ECCOMAS 98, Wiley, 1998.
15. G. Schrauf, J. Perraud, F. Lam, Comparison of boundary layer transition predictions using free flight test data, Journal of Aircraft 35 (6) (1998) 891-897.
16. G. Schrauf, An efficient solver of the eigenvalue problem of the linear stability equations for three-dimensional, compressible boundary layer flows, 6th DGLR-Fach-Symposium (Strömungen mit Ablösung), 8-9.11.1988, Braunschweig, DGLR-REP. 88-05, pp. 18-27; Editor: Deutsche Gesellschaft für Luft- und Raumfahrt e.V. (DGLR), Bonn, Germany.
17. A.J. Skrokowski, S.A. Orszag, K. Kaups, T. Cebeci, A Fortran Program to Compute and Integrate Disturbance Amplification Rates on Swept, Tapered Laminar Flow Control Wings with Suction, Computer Software Management and Information Center, The University of Georgia, Athens, USA, 1979.
18. A.M.O. Smith, N. Gamberoni, Transition, Pressure Gradient and Stability Theory, Douglas Aircraft Company, Long Beach, Calif. Rep. ES 26388, 1956.
19. N transition prediction in Navier-Stokes methods for airfoils, AIAA Journal 37 (10) (1999) 1187-1196.
20. N transition prediction including transitional flow regions, AIAA Journal 38 (11) (2000) 2059-2066.
21. N transition prediction, Journal of Aircraft 39 (1) (2002) 51-58.
22. J.L. van Ingen, A suggested semi-emperical method for the calculation of the boundary-layer transition region, Univ. of Delft, Dept. Aerosp. Eng., Delft, The Netherlands, Rep. VTH-74, 1956.
23. W. Wohlrath, H. Echtle, P. Dick, D. Weite, H.W. Stock, B. Moeken, K.H. Horstmann, R. Müller, C.H. Rohardt, A. Quast, Design and flight test evaluation of a laminar wing glove on a commuter aircraft, ICAS Paper 94-5.4.1, 1994.