Pressure distribution and force measurements on a VTOL tilting wing-propeller model. Part 1: Description and tabulated results

Report (1959)
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Published Date

30-06-1959

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Source:

National Research Council Canada Aeronautical Report LR 252

Abstract

This report presents tabulated results of pressure and force measurements on a half wing model of a twin-engined tilt-wing VTOL configuration over a range of thrust coefficient for a limited range of incidence.

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