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On repetitive flutter calculations in structural designThe use of continually updated natural modes, called changing modes, is discussed together with the employment of fixed modes in the design process. 'No-derivatives' methods are considered. The flutter solution process is separated into parts which are mode dependent and parts which are mode independent. On the basis of this separation an attempt is made to identify the type of design problems which are suitable for the use of changing modes, and the type of problems which are more suitable for fixed modes. The use of derivative methods is also examined.
Document ID
19740036039
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Haftka, R. T.
Yates, E. C., Jr.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 74-141
Report Number: AIAA PAPER 74-141
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 30, 1974
End Date: February 1, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A18789
Distribution Limits
Public
Copyright
Other

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