Aerodynamic Heating of a Gap in the Hypersonic Laminar Boundary Layer

Author:

YOKOI Hironao,KOYAMA Hiroto,NAKAMURA Yoshiaki

Publisher

Japan Society for Aeronautical and Space Sciences

Reference16 articles.

1. 1) Chapman, D.R.: A Theoretical Analysis of Heat Transfer in Regions of Separated Flow, NACA TN 3792, 1956.

2. 2) Burggraf, O.R.: A Model of Steady Separated Flow in Rectangular Cavities at High Reynolds Number, Charwat, A.F., ed., Stanford Univ. Press, 1965, pp.190-229.

3. 3) Throckmorton, D.A.: Heat Transfer to Surface and Gaps of RSI Tile Arrays in Turbulent Flow at Mach 10.3, NASA TM X-71945, April, 1974.

4. 4) Weinstein, I., Avery, D.E. and Chapman, A.J.: Aerodynamic Heating to the Gaps and Surfaces of Simulated Reusable-Surfaces-Insulation Tile Arrays in Turbulent Flow at Mach 6.6, NASA TM X-3225, 1975.

5. 5) Nestler, D.E.: The Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow, AIAA Paper AIAA-85-0971, June 19-21, 1985, Williamsburg Virginia AIAA 20th Thermophysics Conference.

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