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Author: James C. Williams Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 716
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
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
Book Description
This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Author: Richard von Mises Publisher: Courier Corporation ISBN: 0486132226 Category : Technology & Engineering Languages : en Pages : 680
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 : Aeronautics Languages : en Pages : 766
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
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
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.
Author: James C. Williams
Author: James C. Williams
Author: James C. Williams
Author: 
Author: United States. National Aeronautics and Space Administration
Author: George Gerard
Author: Richard von Mises
Author: 
Author: 
Author: K. R. Czarnecki
Author: F. L. Thompson