Performance determined for speeds from 5000 to 14,000 rpm with varying air flow at each speed; determination was in accordance with Committee's recommended procedure for testing superchargers; conclusion was that multistage compressor of high efficiency can be designed by application of airfoil theory. (released 1948) (20¢)
Performance of NACA eight-stage axial-flow compressor designed on basis of airfoil theory
Nat Advisory Committee Aeronautics -- Report
1943
19 pages
Bibliography
Report
Englisch
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Performance of NACA eight-stage axial-flow compressor designed on basis of airfoil theory
Engineering Index Backfile | 1943
|Performance of NACA eight-stage axial-flow compressor at simulated altitudes
Engineering Index Backfile | 1944
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