Results of investigation of full scale, nose slot cowlings conducted in NACA 20-ft wind tunnel to furnish information on pressure drop available for cooling; engine conductances from 0 to 0.12 and exit slot conductances from 0 to 0.30 covered.
Effect of exit-slot position and opening on available cooling pressure for N.A.C.A. Nose-slot cowlings
Nat Advisory Committee Aeronautics -- Report
1940
12 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Flight tests of N.A.C.A. Nose-slot cowlings on BFC-1 airplane
Engineering Index Backfile | 1939
|Full-scale tests of N.A.C.A. Cowlings
Engineering Index Backfile | 1937
|Full-scale tests of N.A.C.A. cowlings
Engineering Index Backfile | 1937
|