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Aerodynamic design trends for commercial aircraftRecent research on advanced-configuration commercial aircraft at DFVLR is surveyed, with a focus on aerodynamic approaches to improved performance. Topics examined include transonic wings with variable camber or shock/boundary-layer control, wings with reduced friction drag or laminarized flow, prop-fan propulsion, and unusual configurations or wing profiles. Drawings, diagrams, and graphs of predicted performance are provided, and the need for extensive development efforts using powerful computer facilities, high-speed and low-speed wind tunnels, and flight tests of models (mounted on specially designed carrier aircraft) is indicated.
Document ID
19860007868
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hilbig, R.
(NASA Headquarters Washington, DC United States)
Koerner, H.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:77976
NASA-TM-77976
Report Number: NAS 1.15:77976
Report Number: NASA-TM-77976
Accession Number
86N17338
Funding Number(s)
CONTRACT_GRANT: NASW-4004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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