Engineering Analysis of Reattaching Shear Layer Heat Transfer

AIAA Journal

Volumn 11, Issue 3, 1973, Pages 390-392

  Nestler, D E ^a  

^a GENERAL ELECTRIC COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS - HYPERSONIC;

HEAT TRANSFER;

EID: 0015600962     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.50476     Document Type: Article

References (10)

1. Nestler, D. E., “An Engineering Analysis of Reattaching Shear Layer Heat Transfer,” AIAA Paper 72-717, Boston, Mass., 1972.
2. Donaldson, C. duP., private communication, Feb. 1969.
3. Kim, B. S. C. and Parkinson, T. W., “Flap Turbulent Heating Characteristics Obtained from a Hypersonic Shock Tunnel,” Journal of Spacecraft and Rockets, Vol. 9, No. 4, April 1972, pp. 227-228.
4. King, H. H. and Baum, E., “Enthalpy and Atom Profiles in the Laminar Separated Shear Layer,” RN-8, March 1963, Electro-Optical Systems Inc. Pasadena, Calif.
5. t = 1) Jet Mixing Between Two Compressible Streams at Constant Pressure,” NASA CR-419, April 1966.
6. Alber, I. E. and Lees, L., “Integral Theory for Supersonic Turbulent Base Flows,” AIAA Journal, Vol. 6, No. 7, July 1968, pp. 1343-1351.
7. Glauert, M. B., “The Wall Jet,” Journal of Fluid Mechanics, Vol. 1, 1956, pp. 625-643.
8. Akfirat, J. C., “Transfer of Heat from an Isothermal Flat Plate to a Two-Dimensional Wall Jet,” Proceedings of the 3rd International Heat Transfer Conference. AlChE, New York. Vol. 2, 1966, pp. 274-279.
9. Holden, M. S., "Experimental Studies of Separated Flows at Hypersonic Speeds. Part 2: Two-Dimensional Wedge Separated Flow Studies,” AIAA Journal, Vol. 4, No. 5, May 1966, pp. 790-799.
10. Holden, M. S., “Shock Wave—Turbulent Boundary Layer Interaction in Hypersonic Flow,” AIAA Paper 72-74, San Diego, Calif., 1972.