Note on the Concept of Blunt Trailing Edge Blades
1967
37 pages
Report
No indication
English
Jet & Gas Turbine Engines , Axial compressor , Blunt body , Supersonic flow , Trailing edge , Axial , Blade , Blunt , Body , Compressor , Deceleration , Edge , Flow , Ratio , Rotor , Subsonic , Supersonic , Tip , Trailing , Transonic
Note on the Concept of Blunt Trailing Edge Blades
NTIS | 1967
|Analysis of Blunt Trailing Edge Airfoils
AIAA | 2003
|Trailing Edge Blowing of Fan Blades
AIAA | 2005
|Navier-Stokes analysis of blunt trailing edge airfoils
AIAA | 1992
|