Natural Laminar Flow Airfoil Design Considerations for Winglets on Low-speed Airplanes PDF Download

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Natural Laminar Flow Airfoil Design Considerations for Winglets on Low-speed Airplanes

Natural Laminar Flow Airfoil Design Considerations for Winglets on Low-speed Airplanes PDF Author: Cornelis P. Van Dam
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24
Book Description

Natural Laminar Flow Airfoil Design Considerations for Winglets on Low-speed Airplanes

Natural Laminar Flow Airfoil Design Considerations for Winglets on Low-speed Airplanes PDF Author: Cornelis P. Van Dam
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24
Book Description


1979 NASA authorization (program review)

1979 NASA authorization (program review) PDF Author: United States. Congress. House. Committee on Science and Technology. Subcommittee on Space Science and Applications
Publisher:
ISBN:
Category :
Languages : en
Pages : 436
Book Description


1979 NASA Authorization

1979 NASA Authorization PDF Author: United States. Congress. House. Committee on Science and Technology
Publisher:
ISBN:
Category :
Languages : en
Pages : 450
Book Description


Natural Laminar Flow Airfoil Design Considerations for Winglets on Low-speed Airplanes

Natural Laminar Flow Airfoil Design Considerations for Winglets on Low-speed Airplanes PDF Author: C. P. Vandam
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Winglet airfoil section characteristics which significantly influence cruise performance and handling qualities of an airplane are discussed. A good winglet design requires an airfoil section with a low cruise drag coefficient, a high maximum lift coefficient, and a gradual and steady movement of the boundary layer transition location with angle of attack. The first design requirement provides a low crossover lift coefficient of airplane drag polars with winglets off and on. The other requirements prevent nonlinear changes in airplane lateral/directional stability and control characteristics. These requirements are considered in the design of a natural laminar flow airfoil section for winglet applications and chord Reynolds number of 1 to 4 million.

Low-speed Aerodynamic Characteristics of a 13 Percent Thick Medium Speed Airfoil Designed for General Aviation Applications

Low-speed Aerodynamic Characteristics of a 13 Percent Thick Medium Speed Airfoil Designed for General Aviation Applications PDF Author: R. J. McGhee
Publisher:
ISBN:
Category :
Languages : en
Pages : 88
Book Description


1975 NASA Authorization

1975 NASA Authorization PDF Author: United States. Congress. House. Committee on Science and Astronautics
Publisher:
ISBN:
Category :
Languages : en
Pages : 838
Book Description


1975 NASA Authorization, Hearings Before....

1975 NASA Authorization, Hearings Before.... PDF Author: United States. Congress. House Science and Astronautics Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 744
Book Description


Hearings, Reports and Prints of the House Committee on Science and Astronautics

Hearings, Reports and Prints of the House Committee on Science and Astronautics PDF Author: United States. Congress. House. Committee on Science and Astronautics
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 1702
Book Description


NASA Low- and Medium-speed Airfoil Development

NASA Low- and Medium-speed Airfoil Development PDF Author: Robert J. McGhee
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 24
Book Description


International Science and Technology Transfer Act of 1974

International Science and Technology Transfer Act of 1974 PDF Author: United States. Congress. House. Committee on Science and Astronautics. Subcommittee on International Cooperation in Science and Space
Publisher:
ISBN:
Category : Technical assistance, American
Languages : en
Pages : 2304
Book Description