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X-48B Blended Wing Body Ground to Flight Correlation UpdateThe program objectives are: (1) Assess stability & control characteristics of a Blended Wing Body (BWB) class vehicle in free-flight conditions, (2) Assess flight control algorithms designed to provide desired flight characteristics, and (3) Evaluate prediction and test methods for BWB class vehicles.
Document ID
20110011973
Acquisition Source
Headquarters
Document Type
Presentation
Authors
Vicroy, Dan (NASA Headquarters Washington, DC United States)
Date Acquired
August 25, 2013
Publication Date
January 4, 2011
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
HQ-STI-11-019
Report Number: HQ-STI-11-019
Meeting Information
Meeting: AIAA 2010 Conference
Location: Orlando, FL
Country: United States
Start Date: January 4, 2011
End Date: January 7, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.

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