Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory
1944-08-01
Miscellaneous
No indication
English
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 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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