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Stability characteristics of elastic airplaneSystem of computer programs uses linear theories to evaluate static and dynamic stability, trim state, inertial, and aerodynamic loading, and elastic deformations of aircraft configurations at subsonic and supersonic speeds. Primary emphasis is on analysis of stability and control characteristics of flexible aircraft. System also solves simple rigid aerodynamic problems.
Document ID
19780000092
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Erickson, L. L.
Date Acquired
August 9, 2013
Publication Date
June 1, 1978
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11144
Report Number: ARC-11144
ISSN: 0145-319X
Accession Number
78B10092
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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