Boundary layer transition in hypersonic flows

Author:

MALIK M.1,ZANG T.2,BUSHNELL D.2

Affiliation:

1. High Technology Corp., Hampton, VA

2. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. Mass flow requirements for LFC wing design

2. Progress in Astronautics & Aeronautics;Viscous Drag Reduction D. M.,1990

3. Boundary-Layer Transition," AIAA J., Vol.13,No. 3,March 1975,pp.290-299. Demetriades,A. "Hypersonic Viscous Flow over a Slender Cone, Part 111: Laminar Instability and Transition," AIAA Paper No. 74-535,1974. Stetson, K. F., Thompson, E. R., Donaldson, J. C., and Siler, L. G. "Laminar Boundary Layer Stability Experiments on a Cone at Mach 8, Part 1: Sharp Cone," NAA Paper No. 83-1761, 1983. Malik, M. R. "Prediction and Control of Transition in Supersonic and Hypersonic Boundary Layers,"AIAA J., Vol. 27, No. 11, pp. 1487-1493,1989. Malik, M. R. and Spall, R. E. "On the Stability of Compressible Flow Past Axisymmetric Bodies," High Technology Report No. HTC8905,October 1989. Gapanov, S. A. "The Influence of Flow Non-Parallelism on Disturbances Development in the Supersonic Boundary Layer," Proc. Eighth Canadian Cong. of Appl. Mech., 1981,pp. 673-674. El-Hady, N. M. "On the Effect of Boundary Layer Growth on the Stability of Compressible Flows," NASA CR-3474, 1981. El-Hady, N. and Verma, A. K. "Growth of Gortler Vortices in Compressible Boundary Layers Along Curved Surfaces," AIAA Paper NO.81-1278, 1981. Hall, P. and Malik, M. R. "The Growth of Gortler Vortices in Compressible Boundary Layers," International J. of Eneineering Mathematics,Vol. 23, 1989,pp. 239-251. Spall, R. E. and Malik, M. R. "Goertler Vortices in Supersonic and Hypersonic Boundary Layers," Phvs. Fluids A, Vol. 1, NO.11,November 1989,pp. 1822-1835. Beckwith, I. E. and Holley, B. B. "Gortler Vortices and Transition in Wall Boundary Layers of Two Mach 5 Nozzles," NASA TP1869,August 1981. Chen F. J.,Malik, M. R., and Beckwith, I. E. "Instabilities and Transition in the Wall Boundary Layers of Low Disturbance Supersonic Nozzles," AIAA Paper No. 85-1573, 1985. Creel, T. R., Jr., Malik, M. R., and Beckwith, I. E. "Experimental and Theoretical Investigation of Boundary-Layer Instability Mechanisms on a Swept Leading Edge at Mach 3.5," Research in Natural Laminar Flow and Laminar-Flow Control, NASA Conf. Publication 2487,Part 3,March 1987,pp. 981-995.

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