Thrust vector control, heat transfer modeling
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Author
Contributions
- Naval Postgraduate School (U.S.) - Contributor
Publication
1986 - Naval Postgraduate School, Monterey, California, California
Language
English
Word Count
16,250 words, Guess
Page Count
65 pages
Identifiers
- Internet Archivethrustvectorcont00leit
- OCLC Control Number78991489
- Open LibraryOL25484566M
Description
The report presents heat transfer modeling of Thrust Vector control systems using the PHOENICS computer code. Simple two-dimensional wedge and blunt bodies have been examined in supersonic cold flow, for both laminar and turbulent flow cases. The research presents a numerical solution of the supersonic compressible viscous two-dimensional flow field. Post calculations were done to estimate skin friction coefficient, surface heat flux, heat transfer coefficient and Stanton number distributions in both wedge and blunt cases.
Subjects
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