An experimental investigation of leading edge shock wave-boundary layer interaction at hypersonic speeds

An experimental investigation of leading edge shock wave-boundary layer interaction at hypersonic speeds

NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document. The boundary layer on a slender body tends to be very thick at hypersonic speeds. It interacts with the external flow by producing larger flow deflections near the leading edge than t...

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Bibliographic Details
Main Author: Kendall, James Madison
Format: Others
Published: 1956
Online Access:https://thesis.library.caltech.edu/1112/1/Kendall%2Cjr_jm_1956.pdf
Kendall, James Madison (1956) An experimental investigation of leading edge shock wave-boundary layer interaction at hypersonic speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/6XVK-B331. https://resolver.caltech.edu/CaltechETD:etd-03252004-153340 <https://resolver.caltech.edu/CaltechETD:etd-03252004-153340>

Internet

https://thesis.library.caltech.edu/1112/1/Kendall%2Cjr_jm_1956.pdf
Kendall, James Madison (1956) An experimental investigation of leading edge shock wave-boundary layer interaction at hypersonic speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/6XVK-B331. https://resolver.caltech.edu/CaltechETD:etd-03252004-153340 <https://resolver.caltech.edu/CaltechETD:etd-03252004-153340>

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