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Developments in the NASA transport aircraft laminar flow programThe NASA transport aircraft laminar flow program is assessed including on-going work and future research. The on-going program is discussed with reference to the advanced swept LFC airfoil tests, wind surface panel development, and leading edge flight tests. Among the areas of research considered are the variable sweep transition flight test, laminar flow wing aerodynamic design, and efficient laminar flow structures.
Document ID
19830035296
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wagner, R. D. (NASA Langley Research Center Hampton, VA, United States)
Fischer, M. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 83-0090
Report Number: AIAA PAPER 83-0090
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Reno, NV
Start Date: January 10, 1983
End Date: January 13, 1983
Accession Number
83A16514
Distribution Limits
Public
Copyright
Other

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