A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft PDF Download
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Author: James C. Williams
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 716
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Book Description
This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Author: James C. Williams
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 716
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Book Description
This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Author: James C. Williams
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 734
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Book Description
This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 230
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Book Description
Author: George Gerard
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 28
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Book Description
Author: Richard von Mises
Publisher: Courier Corporation
ISBN: 0486132226
Category : Technology & Engineering
Languages : en
Pages : 680
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Book Description
Mises' classic avoids the formidable mathematical structure of fluid dynamics, while conveying — by often unorthodox methods — a full understanding of the physical phenomena and mathematical concepts of aeronautical engineering.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 492
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 766
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Book Description
Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Author: K. R. Czarnecki
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 20
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Book Description
An investigation has been made in the Langley full-scale tunnel to determine the thickness and shape of profile of the boundary layer on the fuselage of a typical monoplane fighter airplane with a single liquid-cooled engine. The results showed that, for the range of angles of attack and fuselage stations investigated, the maximum displacement thickness was nearly 1.2 inches and was at the most rearward station (81.6 percent of the fuselage length). The displacement thickness was found to be greatly affected by the pressure gradients over the windshield-canopy combination and in the wing-fuselage juncture. An average value for the shape parameter between 1.3 and 1.4 was obtained for the turbulent boundary layer.
Author: F. L. Thompson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 566
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Book Description
It may be concluded that the stalling of vertical tail surfaces is not in itself a dangerous condition. Provided sufficient directional stability exists at large angles of sideslip, the tail stall may occur with modern airplanes, as with those of the past, without the knowledge of or concern to the pilot.
