California Institute of Technology > Image Archive > Hypersonic flow

Image / Hypersonic flow

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Title
Hypersonic flow
Contributing Institution
California Institute of Technology
Collection
Image Archive
Rights Information
Materials from the Caltech Archives are made available online for research purposes. Permission for reproduction, distribution, public display, performance, or publication must be obtained in writing from the Head of Archives. The Caltech Archives makes no representation that it is the copyright owner in all of its holdings. It is the responsibility of the user to obtain all necessary rights and clearances for use of materials. For questions, contact Head of Archives.
Description
Shock waves about a cone in the hypersonic wind tunnel at a Mach number of 5.8. the crossed waves are not in the airstream.
No Date
Type
Image
Format
Photographs
Identifier
ct1:4339
http://archives-dc.library.caltech.edu/islandora/object/ct1%3A4339

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