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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
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Robert N Desmarais
(Langley Research Center Hampton, United States)
Robert M Bennett
(Langley Research Center Hampton, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1978
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Computer Programming and Software
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.
Keywords
Flutter
Unsteady Aerodynamics
Vibration Modes
Subsonic Flow
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