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Aircraft equilibrium spin characteristicsProgram provides analytic solutions to nonlinear equations of motion describing spin conditions. Stability characteristics also are determined. Program can be used to study effects of aerodynamic and inertial parameters on spin and could be modified to compute equilibrium conditions for steady maneuvers. Program is written in FORTRAN IV for batch execution on CYBER 173.
Document ID
19800000087
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Adams, W. M., Jr.
Date Acquired
August 10, 2013
Publication Date
August 1, 1980
Publication Information
Publication: NASA Tech Briefs
Volume: 5
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12502
Report Number: LAR-12502
ISSN: 0145-319X
Accession Number
80B10087
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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