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Control Laws for a Wind Tunnel Free-Flight Study of a Blended-Wing-Body AircraftThis paper documents the control laws used in the free-flight tests of a 5% scaled blended-wing-body aircraft in the NASA Langley 30x60 Full-Scale Tunnel, conducted in the summer of 2005.
Document ID
20060051445
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Jackson, E. Bruce (NASA Langley Research Center Hampton, VA, United States)
Buttrill, c. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2006
Subject Category
Aircraft Stability And Control
Report/Patent Number
L-19273
NASA/TM-2006-214501
Funding Number(s)
WBS: WBS 754-02-07-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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