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Aerodynamic Analysis of Low-Speed Wing-Flap SystemsSUBAERF program developed for aerodynamic analysis and design of lowspeed wing-flap systems. SUBAERF based on linearized theory lifting-surface solution. Low speed aerodynamic analysis method used in SUBAERF provides estimates of wing performance which include effects of attainable leading edge thrust and vortex lift.
Document ID
19840000124
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Carlson, H. W. (Kentron International, Inc.)
Walkley, K. B. (Kentron International, Inc.)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13116
ISSN: 0145-319X
Report Number: LAR-13116
Accession Number
84B10124
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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