Design of an Effective Subsonic Wing Cross-Section Using Viscous-Inviscid Interactive Method
International Conference on Innovative Design, Analysis and Development Practices in Aerospace and Automotive Engineering ; 2014 ; Chennai
2014
Aufsatz (Konferenz)
Englisch
Design of an Effective Subsonic Wing Cross-Section Using Viscous-Inviscid Interactive Method
Springer Verlag | 2014
|Numerical solution of subsonic viscous-inviscid interacting flows
Tema Archiv | 1976
|A viscous-inviscid interactive compressor calculation
AIAA | 1978
|