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Engineering & TechnologyContinuous-output terminal-shock-position sensor for mixed-compression inlets evaluated in wind-tunnel tests of YF-12 aircraft inletMiles O DustinContinuous-output terminal-shock-position sensor for mixed-compression inlets evaluated in wind-tunnel tests of YF-12 aircraft inlet

Continuous-output terminal-shock-position sensor for mixed-compression inlets evaluated in wind-tunnel tests of YF-12 aircraft inlet

Miles O Dustin

Engineering & TechnologyEnglish
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“Continuous-output terminal-shock-position sensor for mixed-compression inlets evaluated in wind-tunnel tests of YF-12 aircraft inlet” by Miles O Dustin: a…

Catalogue details

Author
Miles O Dustin
Category
Engineering & Technology
Language
English
Source
HathiTrust

About this book

“Continuous-output terminal-shock-position sensor for mixed-compression inlets evaluated in wind-tunnel tests of YF-12 aircraft inlet” is a book by Miles O Dustin in the “Engineering & Technology” category, written in English. It is in the public domain, so you can read it for free from the open source using the buttons above. If you enjoyed it, press Like to help others find it. Similar books are listed below.

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