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Author:
William Devenport 
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| Description: |
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This calculator is designed to replace tables (e.g. NACA 1135) in performing basic compressible aerodynamics calculations. It is designed for those learning, teaching or using compressible aerodynamics. It computes (both forward and backward) isentropic flow, normal shock and oblique shock relations. It also has a scratch pad for doing the additional arithmetic usually needed to solve compressible aero problems.
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| More information about this material: |
Primary Audience:
College General Ed
Mobile Compatibility:
Not specified at this time
Language:
English
Cost Involved:
no
Source Code Available:
yes
Accessiblity Information Available:
no
Copyright:
yes
Creative Commons:
unsure
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