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Finite volume calculation of three-dimensional potential flow around a propellerThe finite volume scheme of Jameson (1977) is used to calculate potential flow around a propeller rotating at high speed. An H-type mesh is generated and used successfully in the calculations. A test calculation with a thick blade cross section shows that the present code is capable of computing the propeller flow at the advance Mach number 0.8. The possible physical mechanisms which may play an important role in the propeller aerodynamics are discussed.
Document ID
19820048398
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jou, W.-H. (Flow Industries, Inc. Kent, WA, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 82-0957
Meeting Information
Meeting: Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference
Location: St. Louis, MO
Start Date: June 7, 1982
End Date: June 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics and American Society of Mechanical Engineers
Accession Number
82A31933
Funding Number(s)
CONTRACT_GRANT: NAS3-22148
Distribution Limits
Public
Copyright
Other

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