2 edition of Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude found in the catalog.
Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude
David M Straight
Published
1983 by National Aeronautics and Space Administration Scieentific and Technical Information Branch, For sale by the National Technical Information Service] in Washington D.C, [Springfield, Va .
Written in English
Edition Notes
| Statement | David M. Straight and Richard R. Cullom |
| Series | NASA technical paper -- 2171 |
| Contributions | Cullom, Richard R, Lewis Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch |
| The Physical Object | |
|---|---|
| Pagination | 36 p. : |
| Number of Pages | 36 |
| ID Numbers | |
| Open Library | OL14933382M |
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