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User's Guide for a Modular Flutter Analysis Software System (Fast Version 1.0)The use and operation of a group of computer programs to perform a flutter analysis of a single planar wing are described. This system of programs is called FAST for Flutter Analysis System, and consists of five programs. Each program performs certain portions of a flutter analysis and can be run sequentially as a job step or individually. FAST uses natural vibration modes as input data and performs a conventional V-g type of solution. The unsteady aerodynamics programs in FAST are based on the subsonic kernel function lifting-surface theory although other aerodynamic programs can be used. Application of the programs is illustrated by a sample case of a complete flutter calculation that exercises each program.
Document ID
19780020158
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Desmarais, R. N.
(NASA Langley Research Center Hampton, VA, United States)
Bennett, R. M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1978
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-78720
Accession Number
78N28101
Funding Number(s)
PROJECT: RTOP 505-02-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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