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Two degree-of-freedom flutter solution for a personal computerA computer programmed flutter solution has been written in the BASIC language for a personal computer. The program is for two degree-of-freedom bending torsion flutter applications and utilizes two dimensional Theodorsen aerodynamics. The aerodynamics were modified to include approximations for Mach number (compressibility) effects and aspect ratio (finite span) effects. Input options, user instructions, program listing, and a test case application are included.
Document ID
19850014068
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Turnock, D. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1985
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:86381
NASA-TM-86381
Report Number: NAS 1.15:86381
Report Number: NASA-TM-86381
Accession Number
85N22379
Funding Number(s)
PROJECT: RTOP 505-33-43-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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