Last edited by Kesida
Thursday, April 23, 2020 | History

3 edition of Technology for pressure-instrumented thin airfoil models found in the catalog.

Technology for pressure-instrumented thin airfoil models

D. A. Wigley

Technology for pressure-instrumented thin airfoil models

  • 137 Want to read
  • 15 Currently reading

Published by National Aeronautics and Space Administration, Scientific and Technical Information Division, For sale by the National Technical Information Service] in [Washington, DC], [Springfield, Va .
Written in English

    Subjects:
  • Aerofoils.

  • Edition Notes

    Other titlesTechnology for pressure instrumented thin airfoil models.
    StatementDavid A. Wigley.
    SeriesNASA contractor report -- 4173., NASA contractor report -- NASA CR-4173.
    ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17571505M


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Technology for pressure-instrumented thin airfoil models by D. A. Wigley Download PDF EPUB FB2

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Technology for pressure-instrumented thin airfoil models eBook: National Aeronautics and Space Administration NASA: menards.club: Kindle StoreAuthor: National Aeronautics and Space Administration NASA. Wigley, D. A.: Technology For Pressure Instrumented Thin Airfoil Models. NASA CRContract NASI, May NASA CRContract NASI Author: Pierce L.

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Along the X axis is time, and on the y axis is the count of editions published. Technology for pressure-instrumented thin airfoil models / (Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Division, ), by David A. Wigley and Langley Research Center (page images at HathiTrust).

Summer Opening Hours: Our opening hours will be changing between Tuesday 24 December and Wednesday 1 January All reading rooms will be closed from. Sponsor a Book. National Aeronautics and Space Administration, Scientific and Technical Information Division Publisher - works / 1 ebook.

Catalog of infrared observations Daniel Y. Gezari Technology for pressure-instrumented thin airfoil models D. Wigley Read. Elevators (Airplanes) See also what's at Wikipedia, your library, or elsewhere.

Broader terms: Aerofoils; Airplanes -- Control surfaces; Airplanes -- Tail surfaces; Used for: Stabilizers (Airplanes). Active Trailing-Edge Flap Control of Oscillating-Wing Tip Vortex a quasi-steady thin airfoil theory that includes arbitrary hinge positions for the flap and the tab, and an unsteady lifting.

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Modeling Multi-Layer Matrix Cracking in Thin Walled Composite Rotor Blades Pawar, Prashant M. Ganguli, R. 51,1 Aerodynamic Results of a Pressure-Instrumented Model Rotor Test at the DNW Definition of the Mean Camber Line from Airfoil Shapes Book Review.

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SciTech Connect. Rempe, J. L.; Knudson, D. L.; Lutz, R. The accidents at the. A majority of the airfoil design work to be discussed in this paper is based on the inverse approach; i.e., begin with an airfoil pressure (or velocity) distribution that provides the desired performance, and employ an "inverse" calculation procedure to obtain the corresponding airfoil shape.

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The experiments were conducted in the Transonic Wind tunnel Gottingen (TWG). The TWG is a continuously working facility with a 1 m x 1 m adaptive test-section. The ratio of the tunnel height to the chord of the investigated airfoil models is 1 2 Propeller-Turbinen verbessern die Aussichten für Hubschrauber.

Chronological History Fiscal Year Budget Submission - NASA. Results from tests of a rigid pressure instrumented model models for static wing deformation calculations are discussed and a flutter model of a modem transport are compared with and illustrated by a calculation for the model at M = A flutter calculations from the 3D TSD-VISC code described in static wingtip deflection of m and wingtip.