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Aircraft aerodynamics at high angles of attackAEROX program estimates aircraft aerodynamics to high angles of attack (up to sixty degrees). It estimates coefficients of lift, induced drag, and pitching moment for wings and wing body combinations with or without aft horizontal tail. Both trimmed and untrimmed characters are calculated.
Document ID
19770000225
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Axelson, J. A.
Date Acquired
August 8, 2013
Publication Date
September 1, 1977
Publication Information
Publication: NASA Tech Briefs
Volume: 2
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11133
Accession Number
77B10225
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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