Mark Loomis

Shock-tunnel combustor testing for hypersonic vehicles

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Author

Mark Loomis

Contributions

United States. National Aeronautics and Space Administration. - Contributor

Publication

1994 - National Aeronautics and Space Administration, San Jose, Calif, California

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

OCLC Control Number32198098
Open LibraryOL17001315M

Alternate Titles

Shock tunnel combustor testing for hypersonic vehicles.

Subjects

Topics

Mach number Engine testsInlet nozzlesHypersonic flow Hypersonic speed Wind tunnel tests Hypersonic inlets

Series Statement

MCAT Institute final report -- 94-07.
[NASA contractor report] -- NASA CR-196836.

Other Editions

Shock-tunnel combustor testing for hypersonic vehiclesMicroformNational Aeronautics and Space Administration1994-01-01

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