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Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude
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- http://id.worldcat.org/fast/803357
- http://id.loc.gov/authorities/subjects/sh2009010920
- http://id.loc.gov/authorities/subjects/sh85002813
- http://id.worldcat.org/fast/803184
- http://id.worldcat.org/fast/803510
- http://id.loc.gov/authorities/subjects/sh85002861
- http://id.loc.gov/authorities/subjects/sh85002908
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- "Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude"@en
- "Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude"