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
|Other titles||An analysis of wave interactions in swept-wing flows.|
|Statement||by Helen L. Reed.|
|Series||NASA-CR -- 173723., NASA contractor report -- NASA CR-173723.|
|Contributions||United States. National Aeronautics and Space Administration., Stanford University. Thermosciences Division.|
|The Physical Object|
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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.
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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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