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Natural laminar flow airfoil analysis and trade studiesAn analysis of an airfoil for a large commercial transport cruising at Mach 0.8 and the use of advanced computer techniques to perform the analysis are described. Incorporation of the airfoil into a natural laminar flow transport configuration is addressed and a comparison of fuel requirements and operating costs between the natural laminar flow transport and an equivalent turbulent flow transport is addressed.
Document ID
19820007145
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
May 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-159029
B-7220
Accession Number
82N15018
Funding Number(s)
CONTRACT_GRANT: NAS1-14742
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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