Control system concept for an axisymmetric supersonic inlet.

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Bibliographic Details
Title: Control system concept for an axisymmetric supersonic inlet.
Authors: Chun, K. S., Burr, R. H.
Source: Journal of Aircraft; July 1969, Vol. 6, p306-311, 6p
Database: Applied Science & Technology Source
Description
ISSN:00218669