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Aerodynamics on a transport aircraft type wing-body modelThe DFLR-F4 wing-body combination is studied. The 1/38 model is formed by a 9.5 aspect ratio transonic wing and an Airbus A 310 fuselage. The F4 wing geometrical characteristics are described and the main experimental results obtained in the S2MA wind tunnel are discussed. Both wing-fuselage interferences and viscous effects, which are important on the wing due to a high rear loading, are investigated by performing 3D calculations. An attempt is made to find their limitations.
Document ID
19820022411
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schmitt, V. (NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:76878
NASA-TM-76878
Accession Number
82N30287
Funding Number(s)
CONTRACT_GRANT: NASW-3541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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