The 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.
X-48B Blended Wing Body Ground to Flight Correlation Update
AIAA 2010 Conference ; 2011 ; Orlando, FL, United States
2011-01-04
Miscellaneous
No indication
English