Progress Report on Research Supported by Grants from the Defense Research Board of Canada, 1955-1956 PDF Download
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Author: University of Toronto. Institute of Aerophysics
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
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Book Description
Author: University of Toronto. Institute of Aerophysics
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
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Book Description
Author: University of Toronto. Institute for Aerospace Studies
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 378
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 124
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 454
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 790
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Book Description
Author: Antonio Ferri
Publisher: Elsevier
ISBN: 1483149420
Category : Technology & Engineering
Languages : en
Pages : 253
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Book Description
Progress in Aeronautical Sciences, Volume 3 deals with topics in the field of aerodynamics. The book covers topics on aerodynamic design, propulsion systems, hypersonic flows laboratories, and gust research. The text is composed of four articles. The first article presents a review of the aspects of aerodynamic design of swept-winged aircraft. The second paper surveys the applications of ducted propellers. Critical reviews of experimental hypersonic facilities are provided in Chapter 3. The last paper focuses on the meteorological and aeronautical aspects of atmospheric turbulence. Aeronautical engineers, pilots, aviators, and students in the field of aerodynamic design will find this book invaluable.
Author:
Publisher:
ISBN:
Category : Union catalogs
Languages : en
Pages : 712
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Author: Canada. Defence Research Board
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
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Author: William A. Page
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 668
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Book Description
The results of the investigation suggest that at transonic speeds and at small angles of attack the calculation of all aerodynamic characteristics of slender, three-dimensional shapes can be made by use of transonic slender-body theory when the pressures on the equivalent body of revolution are Imown, either by experiment, or by an adequate nonlinear theory. From transonic slender-body theory it is deduced that the slenderness required for this application is the same as that required for the successful application of the transonic area rule.
Author: University of Toronto. Institute for Aerospace Studies
Publisher:
ISBN:
Category :
Languages : en
Pages : 1014
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Book Description
