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An Approximate Theoretical Method For Modeling The Static Thrust Performance Of Non Axisymmetric Two Dimensional Convergent Divergent Nozzles
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Source: The Open Library
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1An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles
By Craig A. Hunter
“An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles” Metadata:
- Title: ➤ An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles
- Author: Craig A. Hunter
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles” Subjects and Themes:
- Subjects: ➤ Boundary layer equations - Mathematical models - Performance prediction - Compressible flow - Nozzle efficiency - Nozzle flow - Static thrust - Nozzle design - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL15409817M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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