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Wing Subsonic Aerodynamic Performance EstimatesSolution by iteration estimates performance of twisted and cambered wings of arbitrary planform. SUBAER based on linearized theory lifting-surface solution provides spanwise distribution of theoretical leading edge thrust, in addition to surface distribution of perturbation velocities. Program written in FORTRAN IV.
Document ID
19830000079
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Carlson, H. W. (Kentron International)
Walkley, K. B. (Kentron International)
Date Acquired
August 11, 2013
Publication Date
August 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12987
Report Number: LAR-12987
ISSN: 0145-319X
Accession Number
83B10079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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