Calculation of the performance characteristics of a three-dimensional scramjet nozzle/afterbody system (Q1569354)
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scientific article; zbMATH DE number 1467883
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Calculation of the performance characteristics of a three-dimensional scramjet nozzle/afterbody system |
scientific article; zbMATH DE number 1467883 |
Statements
Calculation of the performance characteristics of a three-dimensional scramjet nozzle/afterbody system (English)
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3 July 2000
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The authors present an efficient package that can be used to adequately predict the characteristics of three-dimensional scramjet nozzle flows taking into account viscous effects. The authors discuss some features of the computational method desined to improve the numerical accuracy, and compare their results with experimental results and with predictions based on the full Navier-Stokes equations.
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three-dimensional scramjet nozzle flows
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hypersonic aircraft
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viscous effects
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