by National Aeronautics and Space Administration, Langley Research Center, For sale by the National Technical Information Service in Hampton, Va, [Springfield, Va .
Written in English
|Other titles||Computations for the sixteen foot transonic tunnel, NASA, Langley Research Center|
|Statement||Charles E. Mercer ... [et al.].|
|Series||NASA technical memorandum -- 86319|
|Contributions||Mercer, Charles E., Langley Research Center.|
|The Physical Object|
Get this from a library! Computations for the foot transonic tunnel, NASA, Langley Research Center. [Charles E Mercer, (Aerospace engineer); Langley Research Center.;]. NASA's Foot Transonic Tunnel Leaves Powerful Legacy When the massive fan blades stop turning for the last time on Septem , the steel walls of the Foot Transonic Tunnel will continue to reverberate with an incredible history of aeronautical research spanning over six decades. Langley's 8-Foot Transonic Pressure Tunnel (TPT) was completed in (on the former site of the Propeller Research Tunnel). The tunnel was capable of operating at pressures between and atmospheres, and had Center: Langley Research Center. NASA Langley Research Center, 8-Foot Transonic Pressure Tunnel, Thornell Avenue, Hampton, Hampton, VA Photo(s): 12 | Data Page(s): 17 | Photo Caption Page(s): 2 Contributor: Newbill, Michael - Anderson, Richard K, Jr - Laird, Matthew R - Mattson, Axel T - Cunningham, Chris - Dutton, David H - National Advisory Committee for Aeronautics - Draley, Eugene C - .
The Collier Trophy recognized a transonic-research-technology advance first applied in the two NACA Langley wind tunnels shown in these midcentury views. 15 Top: Air flows counterclockwise in the Foot Transonic Tunnel, passing repeatedly through the test section linked to the topmost floors of the facility's brick office building. Foot Transonic Tunnel. The Langley Foot Transonic Tunnel (Ft TT) is an atmospheric, closed-circuit tunnel with a Mach number range of to and a Reynolds number range from 1 x 10 6 to 4 x 10 6 per foot. The test section of the tunnel is octagonal with a distance of ft across the flats. Photograph at left is ice research at NASA Glenn Research Center. Ice on wings and other aircraft surfaces has been a maior cause of accidents. A 5, horsepower fan in this tunnel can produce airspeeds up to mph, and a 2,ton cooler can lower the temperature to degrees F inside the Icing Research Tunnel at NASA's Glenn Research Center. NASA Langley to shut down transonic wind tunnel. As part of a national initiative to optimize government-owned wind tunnels, NASA's Langley Research Center will shut down its Foot Transonic Tunnel and transition work to other facilities. The tunnel is scheduled to be put in mothball status Septem
NASA Langley's specialized research facilities enable the center to perform world-class research in aeronautics, atmospheric sciences and space technology. Langley's wind tunnels allow engineers to conduct testing that encompasses the entire speed range from 0 mph to nearly M or approximat mph. NASA Langley Research Center is officially opening the Katherine G. Johnson Computational Research Facility — a $23 million consolidated computer center with so much firepower it’ll be used on. Dr. Danehy develops optical measurement systems in the Advanced Measurements and Data Systems Branch in the Research Directorate at NASA Langley Research Center, Hampton, VA. He develops laser-based measurement techniques to study subsonic, transonic, supersonic and hypersonic wind tunnel flows as well as combustion environments. The Subsonic/Transonic Testing Branch provides comprehensive Wind Tunnel testing services for advanced aerodynamic concept development and assessment, advanced computational fluid dynamics tool validation & verification, and risk reduction for vehicle development of aircraft, rotorcraft, missile, and spacecraft systems for NASA, other US.