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: prepared for Lewis Research Center.
Contributors: Gruber, M.; Parzych, David J.; Lewis Research Center
Publisher: Lewis Research Center
Published: 1988
Place of publication: Cleveland, Ohio
Number of pages: 41
Subjects: Prop-fans
Notes: Includes bibliographical references: p. 16.