Influence of nose forms, skirts, flaps, propellers, spinners, and special blowers investigated; results show comparative inefficiency of adjustable skirt flaps, detrimental effect of small-diameter front openings of cowling, and beneficial effect of carefully designed airfoil section near hub of propeller.
Cooling of airplane engines at low air speeds
Nat Advisory Committee Aeronautics -- Report
1937
10 pages
Report
Englisch
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