Effect of inlet velocity ratio, angle of attack, radiator resistance, and propeller operation on pressure recovery at radiator, on drag of cooling installation, and on critical speed of ducts. (Advance Restricted Report L4H15 Oct 1944)
Full-scale wind-tunnel investigation of forward underslung cooling-air ducts
Nat Advisory Committee Aeronautics -- Wartime Report
1944
19 pages
33 supp plates
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Wind-tunnel investigation of rear underslung fuselage ducts
Engineering Index Backfile | 1943
|Wind-tunnel investigation of rear underslung fuselage ducts
TIBKAT | 1943
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