Unsteady potential flow past a propeller blade section
By: M.A. Takallu.
Contributors: Lockheed Engineering & Sciences Company.; Langley Research Center.
Series: NASA contractor report -- 4307.; NASA contractor report -- NASA CR-4307.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1990
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 25
Subjects: Propellers, Aerial.; Unsteady flow (Aerodynamics); Flow distribution.; Lift.; Potential flow.; Pressure distribution.; Propeller blades.; Unsteady flow.
Notes: Prepared at Lockheed Engineering & Sciences Company for Langley Research Center under Contract NAS1-19000.

Includes bibliograpical references: (p. 19-20).

Also available via Internet from the NASA Technical Report Server web site. Address as of 12/07/05:  http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900014930%5F1990014930.pdf; current access is available via PURL.

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