Investigation of the transmission of a shock wave through an orifice

Investigation of the transmission of a shock wave through an orifice

A shock wave propagating in air in a shock tube was reflected from an orifice plate, and the strength or Mach number of the transmitted wave was measured for a range of incident shock Mach numbers from 3 to 9 for several types of orifices. Also schlieren photographs of the starting flow pattern were...

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Bibliographic Details
Main Author: Monroe, Louis L.
Format: Others
Published: 1959
Online Access:https://thesis.library.caltech.edu/3102/1/Monroe_ll_1959.pdf
Monroe, Louis L. (1959) Investigation of the transmission of a shock wave through an orifice. Engineer's thesis, California Institute of Technology. doi:10.7907/Y42Q-9F44. https://resolver.caltech.edu/CaltechETD:etd-08122005-134039 <https://resolver.caltech.edu/CaltechETD:etd-08122005-134039>

Internet

https://thesis.library.caltech.edu/3102/1/Monroe_ll_1959.pdf
Monroe, Louis L. (1959) Investigation of the transmission of a shock wave through an orifice. Engineer's thesis, California Institute of Technology. doi:10.7907/Y42Q-9F44. https://resolver.caltech.edu/CaltechETD:etd-08122005-134039 <https://resolver.caltech.edu/CaltechETD:etd-08122005-134039>

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