Performance of NACA Eight-Stage Axial Flow Compressor at Simulated Altitudes. (Originally issued as Advance Confidential Report E4L21 Dec 1944)
Performance of NACA eight-stage axial-flow compressor at simulated altitudes
Nat Advisory Committee Aeronautics -- Wartime Report
1944
7 pages
Supp plates
Report
English
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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 designed on basis of airfoil theory
Engineering Index Backfile | 1943
|