Large-scale wind-tunnel tests of airplane model with un-swept, aspect-ratio-10 wing, two propellers, and area-suction flaps

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Large-scale wind-tunnel tests of airplane model with un-swept, aspect-ratio-10 wing, two propellers, and area-suction flaps

Large-scale wind-tunnel tests of airplane model with un-swept, aspect-ratio-10 wing, two propellers, and area-suction flaps

Weiberg, J.A. / Griffin, Jr., R.N. / Florman, G.L.

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.

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Title :

Large-scale wind-tunnel tests of airplane model with un-swept, aspect-ratio-10 wing, two propellers, and area-suction flaps

Additional title:

NACA -- Tech Note

Contributors:

Weiberg, J.A. (author) / Griffin, Jr., R.N. (author) / Florman, G.L. (author)

Published in:

NACA -- Technical Note

Publication date :

1958

Size :

76 pages

Type of media :

Report

Type of material :

Print

Language :

English

Keywords :

© Metadata Copyright Elsevier B. V. All rights reserved.

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