Details
- C.H. , SIEVERDING -VKI: The confluence of two supersonic jets at the trailing edge of transonic turbine blades
- E. , STANEWSKY -DFvLR/AVA, FR GERMANY: Shock boundary layer interaction in transonic and supersonic flow
- J., CHAUVIN -VKI: Shock boundary layer interaction in compressor cascades. A review of available data
- F.A.E., BREUGELMANS -VKI: The compressor blade definition
- F.A.E., BREUGELMANS -VKI:The cascade and rotor section performance of a 9'57 cambered DCA airfoil.
Comparison with 2D calculations in the transonic and supersonic flow regime - F.A.E., BREUGELMANS -VKI: The cascade and stator section performance of a 48 cambered DCA airfoil.
Comparison with 2D flow calculations in compressible flow regime
Additional Information
Manufacturer | von Karman Institute for Fluid Dynamics |
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