Comparison of boundary-layer transition predictions using flight test data

Journal of Aircraft

Volumn 35, Issue 6, 1998, Pages 891-897

  Schrauf, Géza ^a,c,e   Perraud, Jean ^b,f   Vitiellot, Domenico ^c,g   Lam, Fung ^c,d  

^a DAIMLER AG   (Germany)

^b ONERA   (France)

^c British Aerospace Airbus Ltd ^*

^d BAE SYSTEMS   (United Kingdom)

^e AIAA   (United States)

^f Department DMAE   (Germany)

^g ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPRESSIBLE FLOW; CORRELATION METHODS; FLUID STRUCTURE INTERACTION; INCOMPRESSIBLE FLOW; LAMINAR FLOW; TRANSITION FLOW;

COMPRESSIBLE STABILITY THEORY;

TRANSPORT AIRCRAFT;

EID: 0032202980     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2409     Document Type: Review

References (8)

1. Arnal, D., and Bulgubure C., "Drag Reduction by Boundary Layer Laminarization," La Recherche Aérospatiale, Vol. 3, 1996, pp. 157-165.
2. Schrauf, G., Perraud, J., Vitiello, D., Lam, F., Stock, H. W., and Abbas, A., "Transition Prediction with Linear Stability Theory - Lessons Learned from the ELFIN F100 Flight Demonstrator," Proceedings of 2nd European Forum on Laminar Flow Technology, AAAF, Paris, France, 1996, pp. 58-71.
3. Schrauf, G., "Stability Analysis of the F100 Flight Experiment - A Second Look," ELFIN II TR 173, Jan. 1996.
4. Schrauf, G., "Transition Prediction Using Different Linear Stability Analysis Strategies," AIAA Paper 94-1848, June 1994.
5. Schrauf, G., "Curvature Effects for Three-Dimensional Compressible Boundary-Layer Stability," Zeitschrift für Flugwissenschaften und Weltraumforschung, Vol. 16, No. 2, 1992, pp. 119-127.
6. Bippes, H., "Instability Features Appearing on Swept Wing Configurations," Laminar-Turbulent Transition, edited by D. Arnal and R. Michel, Springer-Verlag, Berlin, 1990.
7. Deyhle, H., and Bippes, H., "Disturbance Growth in an Unstable Three-Dimensional Boundary Layer and Its Dependence on Environmental Conditions," Journal of Fluid Mechanics, Vol. 316, 1996, pp. 73-113.
8. Herbert, T., and Schrauf, G., "Crossflow-Dominated Transition in Flight Tests," AIAA Paper 96-0185, Jan. 1996.