The CAS22 computer program developed to provide for fast design and analysis of shock free airfoil cascades. CAS22 applicable to aerodynamic analysis and transonic shock free redesign of existing two-dimensional cascades of airfoils. Program is written in FORTRAN IV.
Shock Free Airfoil Cascades
NASA Tech Briefs ; 7
1983-08-01
Sonstige
Keine Angabe
Englisch
Theory of unstaggered airfoil cascades in compressible flow
Engineering Index Backfile | 1947
|Exploring the Limits of Shock-free Transonic Airfoil Design
British Library Conference Proceedings | 2005
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