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3 edition of Six-month progress report on an analysis of wave interactions in swept-wing flows found in the catalog.

Six-month progress report on an analysis of wave interactions in swept-wing flows

Six-month progress report on an analysis of wave interactions in swept-wing flows

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Published by National Aeronautics and Space Administration in [Washington, D.C.? .
Written in English

    Subjects:
  • Airplanes -- Wings.

  • Edition Notes

    Other titlesAn analysis of wave interactions in swept-wing flows.
    Statementby Helen L. Reed.
    SeriesNASA-CR -- 173723., NASA contractor report -- NASA CR-173723.
    ContributionsUnited States. National Aeronautics and Space Administration., Stanford University. Thermosciences Division.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15317757M

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    Experimental evidence indicates the presence of a triad resonance interaction between traveling crossflow modes in a swept wing flow. Results indicate that this interaction occurs when the stationary and traveling crossflow modes have similar and relatively low amplitudes (~1% to 6% of the total freestream velocity). IIBA" and the IIBA" logo are registered trademarks owned by International Institute of Business Analysis. %tMC Publications, Inc. Phone: F a: E-mail: [email protected] This and all editions of this book are dedicated to Rita Mulcahy. Her vision made RMC the company it is today. She had a profound influence on so many.

    Analysis of wing-body interaction flutter for a preliminary space shuttle design / (Washington, D.C.: National Aeronautics and Space Administration ; [Springfield, Va.: For sale by the National Technical Information Service], ), by Richard R. Chipman, Peter Shyprykevich, Langley Research Center, and Grumman Aerospace Corporation (page. Full text of "NASA Technical Reports Server (NTRS) An annotated bibliography on transonic flow theory" See other formats.


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Six-month progress report on an analysis of wave interactions in swept-wing flows Download PDF EPUB FB2

Two theoretical approaches are discussed in the next section to model the crossflow/T-S interaction (characteristic of swept wings) as a secondary in- stability.

The first involves the weakly nonlinear combination of crossflow vortices with various oblique-wave solutions to the linear disturbance equa- tions. Get this from a library. Six-month progress report on an analysis of wave interactions in swept-wing flows. [Helen L Reed; United States.

National Aeronautics and Space Administration.; Stanford University. Thermosciences Division.]. Visually Saric and Yeates observe vortices at the wavelength predicted by linear theory; however, in their hot‐wire measurements they find that the second harmonic dominates disturbance growth, with eventually three times the amplitude of the primary wave.

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Each of the nine sections begins with a description of the sea. Part of the Notes on Numerical Fluid Mechanics and Multidisciplinary Design book series (NNFM, volume ) Summary The global linear stability of compressible flow in the leading-edge region of a swept wing is studied using an iterative eigenvalue : Christoph J.

Mack, Peter J. Schmid, Jörn Sesterhenn. Computing Systems in Engineering Vol. 3, Nospp./92 $ + Printed in Great Britain. Pergamon Press Ltd STRUCTURAL NON-LINEARITY EFFECTS ON FLUTTER OF A SWEPT WING IN TRANSONIC FLOWS I. TJATRA, R. KAPANIA and B. GROSSMAN Department of Aerospace and Ocean Engineering, Virginia Cited by: 2.

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