NASA's Advanced Air Transport Technology Project and Boeing tested a 4.5-percent scale model of a Transonic Truss Braced Wing, TTBW, aircraft concept in the 11-Foot Transonic Wind Tunnel at NASA's Ames Research Center in California. Force, moment and surface pressure data were obtained with the use of multiple optical measurement techniques. Model component build-up data and drag-rise data were obtained on both baseline strut and alternate strut configurations.
Understanding aerodynamics for small, large craft
Aerospace America ; 54 , 11
2016
Aufsatz (Zeitschrift)
Englisch
Aerodynamics of High Speed Multihull Craft
British Library Conference Proceedings | 1997
|Online Contents | 2005