Impact pressure and total temperature interpretation at hypersonic mach number

Impact pressure and total temperature interpretation at hypersonic mach number

Results are presented of an experimental investigation of impact-pressure and total-temperature interpretation at a nominal Mach number of 5.6. The data indicate that the Rayleigh equation, which assumes non-viscous flow, requires correction at low free-stream Reynolds numbers. These viscous effects...

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Bibliographic Details
Main Author: Graves, J. C.
Format: Others
Published: 1954
Online Access:https://thesis.library.caltech.edu/5039/1/Graves_jc_1954.pdf
Graves, J. C. (1954) Impact pressure and total temperature interpretation at hypersonic mach number. Engineer's thesis, California Institute of Technology. doi:10.7907/V04Q-TF29. https://resolver.caltech.edu/CaltechETD:etd-12182003-100211 <https://resolver.caltech.edu/CaltechETD:etd-12182003-100211>

Internet

https://thesis.library.caltech.edu/5039/1/Graves_jc_1954.pdf
Graves, J. C. (1954) Impact pressure and total temperature interpretation at hypersonic mach number. Engineer's thesis, California Institute of Technology. doi:10.7907/V04Q-TF29. https://resolver.caltech.edu/CaltechETD:etd-12182003-100211 <https://resolver.caltech.edu/CaltechETD:etd-12182003-100211>

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