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A new blade element method for calculating the prformance of high and intermediate solidity axial flow fans/

Main Author:	Borst, Henry V.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Ames Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978
Series:	NASA contractor report 3063
Subjects:	Propellers, Aerial Airplanes > Turbojet engines

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