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Reduction of Aircraft Cruise Drag By Using Boundary Layer Heating To Minimize Fuselage Skin FrictionThe data reduction and results of the F-15B Flight Test Fixture experiment conducted at NASA Dryden are discussed. In addition, the feasibility of using the Orbital Sciences L-1011 was studied and a cost estimate prepared. Initial discussions have begun with Edwards Flight Research to explore the possibility of using their T-39 aircraft for the second flight experiment.
Document ID
19980004665
Acquisition Source
Armstrong Flight Research Center
Document Type
Contractor Report (CR)
Authors
Kramer, Brian R.
(Eidetics International, Inc. Torrance, CA United States)
Date Acquired
September 6, 2013
Publication Date
November 28, 1997
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:206450
NASA/CR-97-206450
Report Number: NAS 1.26:206450
Report Number: NASA/CR-97-206450
Funding Number(s)
CONTRACT_GRANT: NAS4-50089
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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