Continuoous-Output Terminal-Shock-Position Sensor for mixed-Compression Inlets Evaluated in Wind-Tunnel Tests of YF-12 Aircraft inlet; NASA Technical Memorandum X-3144

Dustin, Miles O; Cole. Neiner

Published by NASA, Wash. D.C., 1974
Language: English
Condition: Used - Very good Soft cover

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Used - Soft cover

Condition: Used - Very good

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