Hypersonic laminar heat transfer
By: by Gustav J. Hokenson
Contributors: Naval Postgraduate School (U.S.)
Publisher: Naval Postgraduate School
Published: 1972
Place of publication: Monterey, California
Language: eng
Number of pages: 22
Subjects: Viscous flow; Transmission; Aerothermodynamics; Heat; Aerodynamic heating
Description: The results of an analog computer study of hypersonic laminar heat transfer including the effects of pressure gradient, mass transfer, velocity slip, Prandtl number, and wall temperature are presented. Reynolds analogy factors and adiabatic wall enthalpy results are included for all combinations of the aforementioned effects. In addition, an auxiliary correlation is presented which simplifies the specification of the Reynolds analogy factor with velocity slip. All the computations were performed on the EAI 580 analog computer. (Author)
Notes: Title from cover.

"October 1972"--Cover.

"NPS-57HW72101A"--Cover.

DTIC Descriptors: Computer aided analysis, pressure gradients.

Author(s) subject terms: Heat transfer, boundary layers, viscous flow, hypersonic flow.

"Approved for public release; distribution unlimited"--Cover.

Technical report; 1972.