Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.

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Bibliographic Details
Main Author:	Wing, David J.
Corporate Author:	Langley Research Center
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1994]
Series:	NASA technical memorandum ; 4574.
Subjects:	Coanda effect. Computational fluid dynamics. Convergent-divergent nozzles. Flow visualization. Fluidics. Secondary flow. Static tests. Thrust vector control. Two dimensional models. Two fluid models. Wind tunnel tests.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:4574
NAS 1.15:4574	Restricted Place a Hold