Computational Fluid Dynamics Investigation of Vortex Breakdown for a Delta Wing at High Angle of Attack

Computational Fluid Dynamics Investigation of Vortex Breakdown for a Delta Wing at High Angle of Attack

by Air Force Institute of Technology (U.S.) (Created by), Jacob A. Freeman

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Product Details

ISBN-13: 9781249401117
Publisher: BiblioScholar
Publication date: 09/17/2012
Pages: 176
Product dimensions: 7.44(w) x 9.69(h) x 0.38(d)

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