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: prepared for Lewis Research Center.
Contributors: Lewis Research Center
Publisher: Lewis Research Center
Published: 1988
Place of publication: Cleveland, Ohio
Format: Microform
Number of pages: 540
Subjects: Prop-fans
Notes: Includes bibliographical references.