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The supersonic triplet - A new aerodynamic panel singularity with directional propertiesA new supersonic triplet singularity has been developed which eliminates internal waves generated by panels having supersonic edges. The triplet is a linear combination of source and vortex distributions which provides the desired directional properties in the flow field surrounding the panel. The theoretical development of the triplet is described, together with its application to the calculation of surface pressure on arbitrary body shapes. Examples are presented comparing the results of the new method with other supersonic panel methods and with experimental data.
Document ID
19790035623
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Woodward, F. A.
(Analytical Methods, Inc. Bellevue, Wash., United States)
Landrum, E. J.
(NASA Langley Research Center Supersonic Aerodynamics Branch, Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 79-0273
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: New Orleans, LA
Start Date: January 15, 1979
End Date: January 17, 1979
Sponsors: American Institute of Aeronautics, Astronautics
Accession Number
79A19636
Funding Number(s)
CONTRACT_GRANT: NAS1-12900
Distribution Limits
Public
Copyright
Other

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