Boundary-layer transition on swept cylinders at hypersonic speeds

AIAA Journal

Volumn 34, Issue 4, 1996, Pages 649-654

  Murakami, Akira ^a,c,d   Stanewskyt, Egon ^b,d,e   Krogmann, Paul ^b,d,e  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

^c Aeroengine Division

^d AIAA ^*

^e Institute for Fluid Mechanics

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000107413     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13123     Document Type: Article

References (11)

1. Poll, D. I. A., "Leading Edge Transition on Swept Wings," AGARD-CP-224, 1977, pp. 21-1-21-11.
2. Poll, D. I. A., "Three-Dimensional Boundary Layer Transition via the Mechanisms of Attachment Line Contamination and Cross Flow Instability," Proceedings of IUTAM Symposium on Laminar-Turbulent Transition (Stuttgart, Germany). Springer-Verlag, Berlin, 1979, pp. 253-362.
3. Poll, D. I. A., "Transition Description and Prediction in Three-Dimensional Flows," AGARD-Rept. 709, June 1984, pp. 5-1-5-23.
4. Bushnell, D. M., and Huffman, J. K., "Investigation of Heat Transfer to a Leading Edge of a 76 Swept Fin With and Without Chordwise Slots and Correlations of Swept-Leading-Edge Transition Data for Mach 2 to 8," NASA TMX-1475, Dec. 1967.
5. Creel, T. R., Jr.. Beckwith, I. E., and Chen, F. J., "Transition on Swept Leading Edges at Mach 3.5." Journal of Aircraft, Vol. 24, No. 10, 1987, pp. 710-717.
6. Arnal, D., Vignau, F., and Juillen, J. C., "Boundary Layer Tripping in Supersonic Flow," Proceedings of IUTAM Symposium on Laminar- Turbulent Transition (Toulouse, France), Springer-Verlag, Berlin, 1989, pp. 669-679.
7. Ludwieg, H., Hottner, T, and Grauer-Carstensen, H., "Der Rohrwindkanal der Aerodynamichen Versuchsanstalt Göttingen," Jahrbuch 1969 der DGLR. DGLR, Göttingen, Germany, 1969, pp. 52-58.
8. Wendt, V., Kreplin, H., Höhler, G., Grosche, F., Krogmann, P., and Simen, M., "Planar and Conical Boundary Layer Stability Experiments at Mach 5," AIAA Paper 93-5112, Nov. 1993.
9. Schöler, H., "Thermal Imaging on Missiles in Hypersonic Flow," AGARD-CP-493, 1990, pp. 29-1-29-A3.
10. Chapman, G. T, "Some Effects of Leading-edge Sweep on Boundary-Layer Transition at Supersonic Speeds," NACA-TN-D-1075, Sept. 1961.
11. Arnal, D., "Laminar-Turbulent Problems in Supersonic and Hypersonic Flows," AGARD-R-761, June 1989, pp. 8-1-8-45.