Removal of Secondary-flow Accumulations in a Two-dimensional Turbine Nozzle Passage by Boundary-layer Bleed
1955-06-30
Sonstige
Keine Angabe
Englisch
Three-dimensional flow field in a turbine nozzle passage
NTRS | 1993
|Supersonic-lnlet Boundary-Layer Bleed Flow
Online Contents | 1996
|Supersonic-inlet boundary-layer bleed flow
AIAA | 1996
|Three-dimensional flow field in a turbine nozzle passage
AIAA | 1993
|