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Theoretical prediction of thick wing and pylon-fuselage-fanpod-nacelle aerodynamic characteristics at subcritical speeds. Part 2: Computer program descriptionThe procedures required to operate the thick wing and pylon-fuselage-fanpod-nacelle computer program are presented. The program computes surface velocities and pressure, section loads, and total configuration loads and pitching moment. Potential flow theory is used to compute the surface pressures and the associated lift, moment, and vortex drag. The skin friction drag is also computed.
Document ID
19750003864
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kojima, J. (Rockwell International Corp. Los Angeles, CA, United States)
Tulinius, J. R. (Rockwell International Corp. Los Angeles, CA, United States)
Date Acquired
September 3, 2013
Publication Date
July 24, 1974
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-137579
Accession Number
75N11936
Funding Number(s)
CONTRACT_GRANT: NAS2-7904
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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