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Author :
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.23/5 ( download)
Download or read book Swept and Delta Wing Sense written by and published by . This book was released on 1955 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. Office of the Chief of Naval Operations. Aviation Training Division
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.97/5 ( download)
Download or read book Swept and Delta Wing Sense written by United States. Office of the Chief of Naval Operations. Aviation Training Division and published by . This book was released on 1955 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : U.S. Navy. Office of the Chief of Naval Operations. The Aviation Training Division
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.93/5 ( download)
Download or read book Swept and Delta Wing Sense written by U.S. Navy. Office of the Chief of Naval Operations. The Aviation Training Division and published by . This book was released on 1955 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 498 pages
Book Rating : 4.50/5 ( download)
Download or read book Naval Aviation News written by and published by . This book was released on 1955 with total page 498 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Alexander Lippisch
Publisher : Iowa State Press
ISBN 13 :
Total Pages : 144 pages
Book Rating : 4.63/5 ( download)
Download or read book The Delta Wing written by Alexander Lippisch and published by Iowa State Press. This book was released on 1981 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt: Den tyske flykonstruktør beskriver her udviklingen og forsøgene med Tailless- og Delta Wing- flytyper.
Author : Richard Shepherd Shevell
Publisher : Pearson Education India
ISBN 13 : 9788177587425
Total Pages : 468 pages
Book Rating : 4.20/5 ( download)
Download or read book Fundamentals of Flight written by Richard Shepherd Shevell and published by Pearson Education India. This book was released on 1989 with total page 468 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 616 pages
Book Rating : 4.07/5 ( download)
Download or read book NASA Technical Note written by and published by . This book was released on 1975 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Source Wikipedia
Publisher : University-Press.org
ISBN 13 : 9781230615875
Total Pages : 64 pages
Book Rating : 4.73/5 ( download)
Download or read book Wing Configurations written by Source Wikipedia and published by University-Press.org. This book was released on 2013-09 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. Pages: 34. Chapters: Biplane, Canard (aeronautics), Channel wing, Closed wing, Delta wing, Eindecker, Flying wing, Forward-swept wing, Gull wing, Military disc-shaped aircraft, Monoplane, Multiplane (aeronautics), NACA Report No. 742, Parasol wing, Shoulder wing, Tailless aircraft, Tandem wing, Three lifting surface aircraft, Triplane, Wing configuration.
Author : Arnold Polak
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.80/5 ( download)
Download or read book On the Hypersonic Flow Past Blunted, Flat Delta Wings written by Arnold Polak and published by . This book was released on 1970 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: The flow of a perfect gas over the slab portion of a blunted delta wing flying at hypersonic speeds is studied. A set of approximate equations is derived and a solution - for an inviscid flow - is obtained. Using this solution as a representation for the inviscid flow problem, a formulation to the laminar boundary-layer equations is presented; one which is applicable to the flow field's azimuthal planes where the crossflow gradients are not too large. Numerical solutions to these boundary-layer equations have been obtained; however, these are restricted to the azimuthal planes and near to the leading edges. The results indicate the presence of a dividing surface streamline since a numerical solution could not be obtained near the centerplane of the wing, where the crossflow velocity is large. (Author).
Author : Don D. Davis (Jr.)
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.82/5 ( download)
Download or read book Loads on Thin Wings at Transonic Speeds written by Don D. Davis (Jr.) and published by . This book was released on 1955 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
