Results 231 to 240 of about 1,127 (258)

Unsteady acoustic wave propagation in a transonic compressor cascade

34th Aerospace Sciences Meeting and Exhibit, 1996
The need for improved performance and reduced noise levels has motivated engineers to assess the effects of flow unsteadiness on the aeroacoustic phenomena present in axial-flow turbomachines. A primary source of adverse aeroacoustic effects (noise) and performance degradation is the aerodynamic interaction between adjacent blade rows.
openaire   +1 more source

Design of compressor cascades

39th Aerospace Sciences Meeting and Exhibit, 2001
B. Kaplan, S. Eyi
openaire   +1 more source

Corner separation control by optimizing blade end slots in a linear compressor cascade

Aerospace Science and Technology, 2021
Yangwei Liu, Lipeng Lu, Xavier Ottavy
exaly  

Flow losses in supersonic compressor cascades

2014
Ph. D.
openaire   +1 more source

Secondary flow and losses in a compressor cascade

1958
Three ways in which secondary flow can be generated in a straight compressor cascade have been investigated. 1. Wakeflow. The inlet flow is characterized by a constant inlet angle and a varying stagnation pressure over the span. 2. Skewed flow. The inlet flow is characterized by a constant stagnation pressure and a varying inlet angle over the span. 3.
openaire   +1 more source

Effects of Vortex Generator Application on the Performance of a Compressor Cascade

Journal of Turbomachinery, 2013
Robert Meyer
exaly  

Investigations of an Axial Flow Compressor with Tandem Cascades

Journal of Engineering for Power, 1980
K Bammert
exaly  

Effective end wall profiling rules for a highly loaded compressor cascade

Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2016
Stephen Spence, Haoguang Zhang, Wuli Chu
exaly  

The synergistic effect between compound lean and aspiration on aerodynamic performance in compressor cascades

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018
Shaowen Chen
exaly  

Experimental investigation on separation control by slot jet in highly loaded compressor cascade

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018
Wang Rugen
exaly