Transonic flows in turbomachinery article pay-per-view, VKI LS 1973-56

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Transonic flows in turbomachinery

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C.H., SIEVERDING: The confluence of two supersonic jets at the trailing edge of transonic turbine blades (sample) +€25.00
E., STANEWSKY: Shock boundary layer interaction in transonic and supersonic flow (sample) +€25.00
J.,CHAUVIN: Shock boundary layer interaction in compressor cascades. A review of available data (sample) +€25.00
F.A.E., BREUGELMANS: The compressor blade definition (sample) +€25.00
F.A.E., BREUGELMANS:The cascade and rotor section performance of a 9'57 cambered DCA airfoil.Comparison with 2D calculations in the transonic and supersonic flow regime (sample) +€25.00
F.A.E., BREUGELMANS: The cascade and stator section performance of a 48 cambered DCA airfoil. Comparison with 2D flow calculations in compressible flow regime (sample) +€25.00

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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

Manufacturer	von Karman Institute for Fluid Dynamics

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