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Accession Number:
AD0679803
Title:
INCREASING NOZZLE THRUST BY FLOW ROTATION,
Descriptive Note:
Corporate Author:
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Report Date:
1968-04-05
Pagination or Media Count:
11.0
Abstract:
An analysis was made of the thrust obtainable with a rotating gas stream. A formula was obtained for the overall thrust.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE