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Measurement of the steady surface pressure distribution on a single rotation large scale advanced prop-fan blade at Mach numbers from 0.03 to 0.78

Measurement of the steady surface pressure distribution on a single rotation large scale advanced prop-fan blade at Mach numbers from 0.03 to 0.78

By Peter R. Bushnell

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Publish Date

1988

Publisher

Lewis Research Center

Language

-

Pages

540

Description:

subjectsProp-fans