Impact pressure and total temperature interpretation at hypersonic mach numbers

Impact pressure and total temperature interpretation at hypersonic mach numbers

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An experimental investigation was undertaken at a nominal Mach number of 5.6 in the GALCIT Hypersonic Wind Tunnel, Leg No. 1. The first phase was an investigation of the viscous effects on measured impact pressures. The second was an investigation of the temperature recovery characteristics of a sin...

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Bibliographic Details
Main Author: Quiel, Norwald R
Format: Others
Published: 1954
Online Access:https://thesis.library.caltech.edu/4789/1/Quiel_nr_1954.pdf
Quiel, Norwald R (1954) Impact pressure and total temperature interpretation at hypersonic mach numbers. Engineer's thesis, California Institute of Technology. doi:10.7907/SMHA-4160. https://resolver.caltech.edu/CaltechETD:etd-12052003-095631 <https://resolver.caltech.edu/CaltechETD:etd-12052003-095631>

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