An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles [microform] / Craig A. Hunter.

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Bibliographic Details
Main Author:	Hunter, Craig A.
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], [1995]
Series:	NASA contractor report ; NASA CR-195050.
Subjects:	Boundary layer equations. Compressible flow. Convergent-divergent nozzles. Mathematical models. Nozzle design. Nozzle efficiency. Nozzle flow. Performance prediction. Static thrust.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:195050
NAS 1.26:195050	Restricted Place a Hold