Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory
1944
35 S., [17] Bl
Ill., graph. Darst
Originally issued August 1944 as Advance confidential report E4H18
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
Englisch
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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