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FLEXSTAB analysisThe wing differential pressure distributions of two vehicles are predicted using FLEXSTAB. Three space shuttle configurations were investigated. Comparisons were made of wind tunnel and analytical data for a selected range of angle of attack, angle of sideslip, and Mach number. A drone-type vehicle was investigated and comparisons were made between flight and analytical data of wing pressure distributions and static longitudinal stability derivatives.
Document ID
19760011965
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lowder, H. E., Jr. (Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-146435
TR-76-M1
Report Number: NASA-CR-146435
Report Number: TR-76-M1
Accession Number
76N19053
Funding Number(s)
CONTRACT_GRANT: NSG-1093
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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