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Sunday, April 19, 2020 | History

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

On-line analysis capabilities developed to support the AFW wind-tunnel tests

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Published 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

    Subjects:
  • Wind tunnels -- Testing.

  • Edition Notes

    Other titlesOn line analysis capabilities developed ....
    StatementCarol D. Wieseman, Sherwood T. Hoadley, and Sandra M. McGraw.
    SeriesNASA technical memorandum -- 107651.
    ContributionsHoadley, Sherwood Tiffany., McGraw, Sandra M., Langley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18055410M


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On-line analysis capabilities developed to support the AFW wind-tunnel tests by Carol D. Wieseman Download PDF EPUB FB2

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Wieseman (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible : Carol D. 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.

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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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