Thrust vector control, heat transfer modeling
by A. Leitner
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.
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Edition Notes
"NPS-69-86-005"--Cover.
Cover title.
"Contractor report"--Cover.
"Prepared for: Naval Postgraduate School, Monterey, California 93943."
"July, 1986"--Cover.
Includes bibliographical references (p. 26).
"Approved for public release; distribution is unlimited"--Cover.
Technical report; 1986.
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