Performance of NACA Eight-Stage Axial-Flow Compressor Designed on Basis of Airfoil Theory. (Originally issued as Advance Confidential Report E4H18 Aug 1944)
Performance of NACA eight-stage axial-flow compressor designed on basis of airfoil theory
Nat Advisory Committee Aeronautics -- Wartime Report
1943
35 pages
Supp plates
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
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
|