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PROPELLER SLIPSTREAM EFFECTS AS DETERMINED FROM WING PRESSURE DISTRIBUTION ON A LARGE-SCALE SIX-PROPELLER VTOL MODEL AT STATIC THRUST

By: Winston,M M.
Contributor(s): Huston,R J.
Material type: materialTypeLabelBookPublisher: Nasa, Washington, D.C. 1962Description: 67.DDC classification: NASA | TN D-1509
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Item type Current location Collection Call number Status Date due Barcode Item holds
Technical Report Technical Report PK Kelkar Library, IIT Kanpur
General Stacks NASA TN D-1509 (Browse shelf) Not for loan Untraceable TR11473
Total holds: 0

Bound With Nasa Tn D-1501-1508.

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