Hypersonic flow over a yawed circular cone

Hypersonic flow over a yawed circular cone

NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document. A 10[degree] semi-apex, circular cone is tested in air at Mach 8 and at yaw angles to 24[degrees]; surface pressure, heat transfer, and pitot-pressure throughout the flow field are p...

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Bibliographic Details
Main Author: Tracy, Richard R.
Format: Others
Published: 1964
Online Access:https://thesis.library.caltech.edu/3903/1/Tracy_rr_1964.pdf
Tracy, Richard R. (1964) Hypersonic flow over a yawed circular cone. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/RMWT-TH67. https://resolver.caltech.edu/CaltechETD:etd-10042002-161203 <https://resolver.caltech.edu/CaltechETD:etd-10042002-161203>

Internet

https://thesis.library.caltech.edu/3903/1/Tracy_rr_1964.pdf
Tracy, Richard R. (1964) Hypersonic flow over a yawed circular cone. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/RMWT-TH67. https://resolver.caltech.edu/CaltechETD:etd-10042002-161203 <https://resolver.caltech.edu/CaltechETD:etd-10042002-161203>

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