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Accession Number:
ADA007396
Title:
Experimental Study of Pilot Losses During the Rotation of Supersonic Flow through Wide Angle in Curvilinear Channels,
Descriptive Note:
Corporate Author:
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Report Date:
1975-02-12
Pagination or Media Count:
23.0
Distribution Statement:
APPROVED FOR PUBLIC RELEASE