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A model of the Transonic Truss-Braced Wing aircraft in a wind tunnel at NASA's Ames Research Center. By early 2019, following extensive wind tunnel testing at NASA Ames Research Center, an optimized truss and more sweep for the 170 ft (52 m) span wing allowed flying higher and faster, up from Mach 0.70–0.75 to Mach 0.80 like current jetliners. [3]
"SUGAR sweetens the deal with Phase 3 results, Phase 4 underway". Innovation Quarterly. Boeing. Eric Ting; Kevin W. Reynolds; Nhan T. Nguyen; Joseph Totah (2014). Aerodynamic Analysis of the Truss-Braced Wing Aircraft Using Vortex-Lattice Superposition Approach (PDF). 32nd AIAA Applied Aerodynamics Conference. NASA Technical Reports Server
It’s called the Transonic Truss-Braced Wing concept, which relies on elongated, thin wings stabilized by diagonal struts that connect the wings to the aircraft. The design’s shape creates less ...
USAF, NASA 1959 Hypersonic, high-altitude flight First crewed hypersonic aircraft; capable of suborbital spaceflight. [25] X-15A-2: North American USAF, NASA 1964 Hypersonic, high-altitude flight Major Pete Knight flew the X-15A-2 to a Mach 6.70, making it the fastest piloted flight of the X-plane program. X-16: Bell USAF 1954
[6] In 2018 a new design of engine inlet liner was flight tested in a successor program, Quiet Technology Demonstrator 3 (QTD3), using acoustic arrays at Moses Lake, Washington. [13] The NASA-designed inlet was installed in the right-hand nacelle of one of Boeing's two 737 MAX 7 prototypes, [14] powered by CFM International LEAP 1B engines. The ...
The NEAT should test a megawatt powertrain in fiscal 2019 before the 2.6-megawatt STARC-ABL ingestion system. Boeing’s Mach 0.78 Truss-Braced wing concept High-speed wind-tunnel testing is planned for fiscal 2019.
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An Experimental Investigation of Three Oblique Wing and Body Combinations at Mach Numbers Between .6 and 1.4, NASA TM X-62256, April 1973; With Graham, A., and Summers, J., Wind Tunnel Test of an F-8 Airplane Model Equipped with an Oblique Wing, NASA TM X-62273, June 1973; With Nisbet, J., Transonic Transport Wings -- Oblique or Swept?