A study of axial compressor blade optimization for operation in the low Reynolds number regime
16th Aerospace Sciences Meeting ; 1978 ; Huntsville , AL , U.S.A.
01.01.1978
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Reynolds number effect on axial-flow compressor performance
TIBKAT | 1949
|Aerodynamics of Low Reynolds Number Axial Compressor Sections (AIAA 2015-1934)
British Library Conference Proceedings | 2015
|