![](/img/cover-not-exists.png)
[ASME ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition - Cologne, Germany (Monday 1 June 1992)] Volume 1: Turbomachinery - Prediction of 2D Viscous Transonic Flow in Compressor Cascades Using a Semi-Empirical Shock/Boundary-Layer Interaction Method
Hoeger, M., Broichhausen, K. D.Year:
1992
Language:
english
DOI:
10.1115/92-gt-277
File:
PDF, 1.65 MB
english, 1992