Lastivka, Ivan. “Raising Gas-Dynamic Stability Margin of Axial and Centrifugal Compressor Stages by Means of Vaned Diffuser Boundary Layer Control”. Aviation 15, no. 3 (October 4, 2011): 76-81. Accessed November 24, 2024. https://jau.vgtu.lt/index.php/Aviation/article/view/4974.