Investigation to determine effects of propeller slipstream on lifts obtainable and flow requirements for suction; it is found that propeller slipstream had no effect on suction flow requirements but suction pressures required increased with thrust coefficient.
Large-scale wind-tunnel tests of airplane model with un-swept, aspect-ratio-10 wing, two propellers, and area-suction flaps
NACA -- Tech Note
1958
76 pages
Report
English
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Engineering Index Backfile | 1958
|Engineering Index Backfile | 1959
|