Hypersonic laminar heat transfer
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Authors
Hokenson, Gustave John
Subjects
Advisors
Date of Issue
1972-10
Date
1972-10
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
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)
Type
Technical Report
Description
Series/Report No
Department
Identifiers
NPS Report Number
NPS-57Hw72101A
Sponsors
Funder
Format
Citation
Distribution Statement
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.