3 edition of On-line analysis capabilities developed to support the AFW wind-tunnel tests found in the catalog.
On-line analysis capabilities developed to support the AFW wind-tunnel tests
Carol D. Wieseman
1992 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||On line analysis capabilities developed ....|
|Statement||Carol D. Wieseman, Sherwood T. Hoadley, and Sandra M. McGraw.|
|Series||NASA technical memorandum -- 107651.|
|Contributions||Hoadley, Sherwood Tiffany., McGraw, Sandra M., Langley Research Center.|
|The Physical Object|
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Wieseman. American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA This paper describes the development of transfer function models for the trailing edge and upper- and lower-spoiler actuators of the Benchmark Active Control Technology (BACT) wind Author: Martin Waszak.
On-line analysis capabilities developed to support the active flexible wing wind-tunnel tests (AFW) wind-tunnel tests. These tools were developed to verify control law execution, to satisfy.
capabilities, primarily because of its large size, heavy gas test medium and transonic speed capabilities. Fig. 1- Aerial photograph of the TDT. The TDT had a significant success within months of coming on-line. In late and early the Lockheed Electra aircraft experienced two catastrophic crashes.
Evidence from these crashes pointed in the. Low-speed aerodynamic tests were carried out on a A aircraft model, designated as model DB1. The tests were performed in the closed 8 m x 6 m test section of the DNW-LLF low-speed wind tunnel.
AIRBUS has adapted a scale model of a A such as to represent the BLADE flying Size: KB. On-line analysis capabilities developed to support the AFW wind-tunnel tests. NASA Technical Reports Server (NTRS) Wieseman, Carol D.; Hoadley, Sherwood T.; Mcgraw, Sandra M.
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On-line analysis capabilities developed to support the AFW wind-tunnel tests. NASA Technical Reports Server (NTRS) Wieseman, Carol D.; Hoadley, Sherwood T.; Mcgraw, Sandra M. A variety of on-line analysis tools were developed to support two active flexible wing (AFW) wind-tunnel tests.
These tools were developed to verify control. “Covered Government support contractor” is defined in (a)(6) as “a contractor under a contract, the primary purpose of which is to furnish independent and impartial advice or technical assistance directly to the Government in support of the Government’s management and oversight of a program or effort (rather than to directly.
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Sara Burgerhartstraat 25 P.O. BoxAE Amsterdam, The Netherlands. Tests of new wing Neal T. Frink of Langley and his associates conducted extensive pioneering wind-tunnel tests designs in indicated a supersonic performance improvement of about 30 percent compared with to evaluate the eﬀects of wing-sweep angle and other geometric characteristics on vortex-ﬂap the basic F At subsonic speeds, the 5/5(2).
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