Evaluation of transition in flight tests using nonlinear parabolized stability equation analysis

Journal of Aircraft

Volumn 33, Issue 3, 1996, Pages 554-560

  Schrauf, Géza ^a,d   Herbert, Thorwald ^b,d   Stuckert, Greg ^c,d  

^a DAIMLER AG   (Germany)

^b The Ohio State University   (United States)

^c DynaFlow Inc   (United States)

^d AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; BOUNDARY VALUE PROBLEMS; DATABASE SYSTEMS; NONLINEAR EQUATIONS; STABILITY;

FLIGHT TESTS; PARABOLIZED STABILITY EQUATIONS; STABILITY THEORY; TOLLMIEN SCHLICHTING DOMINATED TEST; TRANSITION EVALUATION;

AERODYNAMICS;

EID: 0030146273     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46980     Document Type: Review

References (23)

1. Van Ingen, J. L., "A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region," Univ. of Technology, Dept. of Aerospace Engineering, Rept. UTH-74, Delft, The Netherlands, 1956.
2. Smith, A. M. O., and Gamberoni, A. H., "Transition, Pressure Gradient and Stability Theory," Douglas Aircraft Co., Rept. ES26388, El Segundo, CA, 1956.
3. Schrauf, G., Bieler, H., and Thiede, P., "Transition Prediction - The Deutsche Airbus View," Proceedings of the 1st European Forum on Laminar Flow Technology, DGLR Rept. 92-06, 1992, pp. 73-82.
4. Schrauf, G., "Curvature Effects for Three-Dimensional Compressible Boundary Layer Stability," Zeitschrift für Flugwissenschaften und Weltraumforschung, Vol. 16, No. 2, 1992, pp. 119-127.
5. Arnal, D., "Boundary Layer Transition: Predictions Based on Linear Theory," Special Course on Progress in Transition Modelling, AGARD Rept. 793, pp. 2/1-63, 1994.
6. Malik, M. R., "Stability for Laminar Flow Control Design," Viscous Drag Reduction in Boundary Layers, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, Vol. 123, 1990, pp. 3-46.
7. Morkovin, M. V., and Reshotko, E., "Dialogue on Progress and Issues in Stability and Transition Research," edited by D. Arnal and R. Michel, Laminar-Turbulent Transition, Springer-Verlag, Berlin, 1990.
8. Schrauf, G., "Transition Prediction Using Different Linear Stability Analysis Strategies," AIAA Paper 94-1848, June 1994.
9. Herbert, T., "Boundary-Layer Transition - Analysis and Prediction Revisited," AIAA Paper 91-0737, Jan. 1991.
10. Bertolotti, F. P., Herbert, T., and Spalart, P. R., "Linear and Nonlinear Stability of the Blasius Boundary Layer," Journal of Fluid Mechanics, Vol. 242, 1992, pp. 441-474.
11. Bertolotti, F. P., "Linear and Nonlinear Stability of Boundary Layers with Streamwise Varying Properties," Ph.D. Dissertation, Ohio State Univ., Columbus, OH, 1991.
12. Herbert, T., "Parabolized Stability Equations," Special Course on Progress in Transition Modelling, AGARD Rept. 793, pp. 4/1-34.
13. Herbert, T., and Schrauf, G., "Crossflow-Dominated Transition in Flight Tests," AIAA Paper 96-0185, Jan. 1996.
14. Kaups, K., and Cebeci, T., "Compressible Laminar Boundary Layers with Suction on Swept and Tapered Wings," Journal of Aircraft, Vol. 14, No. 7, 1977, pp. 661-667.
15. Elsholz, E., "Ein inverses LISW-Grenzschicht-Verfahren," MBB Technical Rept. TE2-1681, Nov. 1988.
16. Schrauf, G., "COAST2 - A Compressible Stability Code. User's Guide and Tutorial," DA-Rept. EF11-1973, Oct. 1993.
17. Stuckert, G., Herbert, T., and Esfahanian, V., "Stability and Transition on Swept Wings," AIAA Paper 93-0078, Jan. 1993.
18. Schrauf, G., Laburthe, F., and Casalis, G., "Stability Computations on the Long Yawed Cylinder of Poll: Comparison of Stability Codes, Curvature Effects," CERT/ONERA Fiche Technique 2/91, Nov. 1991.
19. Schrauf, G., "Comparison of Local and Global Amplification Rates Computed with the 'Fixed Frequency/Fixed Wave Length' Strategy," ELFIN II TR 142, Jan. 1995.
20. Herbert, T., Stuckert, G., and Esfahanian, V., "Effects of Free-Stream Turbulence on Boundary-Layer Transition," AIAA Paper 93-0488, Jan. 1993.
21. Müller, B., "Experimentelle Untersuchung der Querströmungsinstabilität im linearen und nichtlinearen Bereich des Transitionsgebietes," DLR-Forschungsbericht 90-09, Göttingen, Germany, 1990.
22. Reibert, M. S., Saric, W. S., Carillo, R. B., "Experiments in Nonlinear Saturation of Stationary Crossflow Vortices in a Swept-Wing Boundary Layer," AIAA Paper 96-0184, Jan. 1996.
23. Herbert, T., "Secondary Instability of Boundary Layers," Annual Review Fluid Mechanics, Vol. 20, 1988, pp. 487-526.