Wind Tunnel Investigation Of Ordinary And Split Flaps On Airfoils Of Different Profile

Author : Carl Joseph Wenzinger
Publisher :
ISBN 13 :
Total Pages : 176 pages
Book Rating : 4.29/5 ( download)

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Download or read book Wind-tunnel Investigation of Ordinary and Split Flaps on Airfoils of Different Profile written by Carl Joseph Wenzinger and published by . This book was released on 1936 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Carl Joseph Wenzinger
Publisher :
ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.08/5 ( download)

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Download or read book Wind-tunnel Investigation of Ordinary and Split Flaps on Airfoils of Different Profile written by Carl Joseph Wenzinger and published by . This book was released on 1936 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Abe Silverstein
Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.39/5 ( download)

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Download or read book Wind-tunnel Investigation of Tapered Wings with Ordinary Ailerons and Partial-span Split Flaps written by Abe Silverstein and published by . This book was released on 1937 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Carl Joseph Wenzinger
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.68/5 ( download)

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Download or read book Wind-tunnel Investigation of N.A.C.A. 23012, 23021, and 23030 Airfoils with Various Sizes of Split Flap written by Carl Joseph Wenzinger and published by . This book was released on 1940 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Felicien F. Fullmer Jr
Publisher : Forgotten Books
ISBN 13 : 9780666924346
Total Pages : 28 pages
Book Rating : 4.41/5 ( download)

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Download or read book Wind-Tunnel Investigation of NACA 66(215)-216, 66, 1 212, and 651-212 Airfoils with 0. 20 Airfoil-Chord Split Flaps (Classic Reprint) written by Felicien F. Fullmer Jr and published by Forgotten Books. This book was released on 2018-03-19 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Excerpt from Wind-Tunnel Investigation of Naca 66(215)-216, 66, 1 212, and 651-212 Airfoils With 0. 20 Airfoil-Chord Split Flaps Lanclev Memorial Aeronautical Laboratory National Advisory Committee for Aeronautics Langley Field, Va. About the Publisher Forgotten Books publishes hundreds of thousands of rare and classic books. Find more at www.forgottenbooks.com This book is a reproduction of an important historical work. Forgotten Books uses state-of-the-art technology to digitally reconstruct the work, preserving the original format whilst repairing imperfections present in the aged copy. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in our edition. We do, however, repair the vast majority of imperfections successfully; any imperfections that remain are intentionally left to preserve the state of such historical works.

Author : Carl Joseph Wenzinger
Publisher :
ISBN 13 :
Total Pages : 13 pages
Book Rating : 4.97/5 ( download)

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Download or read book Wind-tunnel Investigation of N.A.C.A. 23012, 23021, and 23030 Airfoils with Various Sizes of Split Flap written by Carl Joseph Wenzinger and published by . This book was released on 1939 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Felicien F. Jr Fullmer
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.04/5 ( download)

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Download or read book Wind-tunnel Investigation of NACA 66(215)-216, 66,1-212, and 65(1)-212 Airfoils with 0.20-airfoil-chord Split Flaps written by Felicien F. Jr Fullmer and published by . This book was released on 1944 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Felicien F. Fullmer
Publisher :
ISBN 13 :
Total Pages : 7 pages
Book Rating : 4.80/5 ( download)

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Download or read book Wind-tunnel Investigation of NACA 66(215)-216, 66,1-212, and 65(1)-212 Airfoils with 0.20-airfoil-chord Split Flaps written by Felicien F. Fullmer and published by . This book was released on 1944 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was carried out in the NACA two-dimensional low-turbulence pressure tunnel of the NACA 66(215)-216, 66,1-212, and 65(sub-1)-212 airfoil sections equipped with split flaps having chords 20 percent of the airfoil chord. The purpose was to determine the maximum-lift characteristics of these low-drag airfoil sections with split flaps. All present tests were made at a Reynolds number of approximately 6,000,000 and a Mach number of about 0.15.

Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 670 pages
Book Rating : 4.17/5 ( download)

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Download or read book Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1934 with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 400 pages
Book Rating : 4.02/5 ( download)

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Download or read book Wartime Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 400 pages. Available in PDF, EPUB and Kindle. Book excerpt: