Measurement of unsteady blade surface pressure on a single rotation large scale advanced prop-fan with angular and wake inflow at mach numbers from 0.02 to 0.70
By: P. Bushnell, M. Gruber, and D. Parzych.
Contributors: Gruber, M.; Parzych, David J.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- 182123.; NASA contractor report -- NASA CR-182123.
Publisher: National Aeronautics and Space Administration
Published: 1990
Place of publication: [Washington, DC]
Language: eng
Format: Microform
Subjects: Propellers.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1990. 1 microfiche.