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Static aerodynamic characteristics of a model with a 17 percent thick supercritical wingThe statis stability and control characteristics and air loads on the wing and aileron of a 0.09 scale model of an airplane with a 17 percent thick supercritical wing were investigated. The longitudinal aerodynamic characteristics were determined over a lift coefficient range sufficiently high to induce buffet onset at Mach numbers from 0.30 to 0.80. In addition, the lateral aerodynamic characteristics were determined as a function of sideslip angle and angle of attack at selected Mach numbers.
Document ID
19830002804
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ferris, J. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-2551
L-8081
NAS 1.15:X-2551
Report Number: NASA-TM-X-2551
Report Number: L-8081
Report Number: NAS 1.15:X-2551
Accession Number
83N11074
Funding Number(s)
PROJECT: RTOP 742-73-02-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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