Performance of NACA eight-stage axial-flow compressor at simulated altitudes
Wartime report ; E-5
1944
7 S., [10] Bl
Ill., graph. Darst
Originally issued December 1944 as Advance confidential report E4L21
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Performance of NACA eight-stage axial-flow compressor at simulated altitudes
Engineering Index Backfile | 1944
|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
|