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Application of a supersonic kernel-function procedure to flutter analysis of thin lifting surfaces

Author: Herbert J Cunningham; United States. National Aeronautics and Space Administration.; Langley Research Center.
Publisher: Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970.
Series: NASA technical note, D-6012.
Edition/Format:   Print book : National government publication : EnglishView all editions and formats
Database:WorldCat
Summary:
A description is presented of a systematic procedure for obtaining generalized aerodynamic forces from the lifting-surface theory by the supersonic kernel-function method and for using those forces thus obtained in a Galerkin modal flutter analysis. The method is applicable to planforms with subsonic leading and supersonic trailing edges. Analytical flutter results were obtained and compared with experimental values  Read more...
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Details

Material Type: Government publication, National government publication, Internet resource
Document Type: Book, Internet Resource
All Authors / Contributors: Herbert J Cunningham; United States. National Aeronautics and Space Administration.; Langley Research Center.
OCLC Number: 57582416
Description: 38 pages : illustrations ; 27 cm.
Series Title: NASA technical note, D-6012.
Responsibility: Herbert J. Cunningham.

Abstract:

A description is presented of a systematic procedure for obtaining generalized aerodynamic forces from the lifting-surface theory by the supersonic kernel-function method and for using those forces thus obtained in a Galerkin modal flutter analysis. The method is applicable to planforms with subsonic leading and supersonic trailing edges. Analytical flutter results were obtained and compared with experimental values from three flutter models.

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Primary Entity

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