Use of low speed and high speed 2-dimensional cascade tunnels and low speed test blower, to determine experimental method of designing blades; important parameters involved in compressor blade design, turning angles or loading, design angle of attack, and qualitative critical speed evaluated.
N.A.C.A. Cascade data for blade design of high-performance axial-flow compressors
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 15 , n 2
1948
7 pages
Aufsatz (Zeitschrift)
Englisch
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