Natural Laminar Flow Airfoil Design Considerations for Winglets on Low-speed Airplanes
Author : Cornelis P. Van Dam
Publisher :
Page : 36 pages
File Size : 16,68 MB
Release : 1984
Category : Airplanes
ISBN :
Author : Cornelis P. Van Dam
Publisher :
Page : 36 pages
File Size : 16,68 MB
Release : 1984
Category : Airplanes
ISBN :
Author : C. P. Vandam
Publisher :
Page : 36 pages
File Size : 43,6 MB
Release : 1984
Category :
ISBN :
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.
Author :
Publisher :
Page : 994 pages
File Size : 34,95 MB
Release : 1995
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 416 pages
File Size : 22,88 MB
Release : 1985
Category : Aeronautics
ISBN :
Author : Michael S. Selig
Publisher : Soartech
Page : 320 pages
File Size : 38,16 MB
Release : 1995
Category : Technology & Engineering
ISBN :
Author :
Publisher :
Page : 340 pages
File Size : 50,72 MB
Release : 1986
Category : Fluid dynamics
ISBN :
Author : Cornelis P. Van Dam
Publisher :
Page : 180 pages
File Size : 50,9 MB
Release : 1983
Category : Aerodynamics
ISBN :
Author : National Aeronautics and Space Administration
Publisher : CreateSpace
Page : 86 pages
File Size : 37,26 MB
Release : 2013-11
Category : History
ISBN : 9781493794324
Laminar-flow control is an area of aeronautical research that has a long history at NASA's Langley Research Center, Dryden Flight Research Center, their predecessor organizations, and elsewhere. In this monograph, Albert L. Braslow, who spent much of his career at Langley working with this research, presents a history of that portion of laminar-flow technology known as active laminar-flow control, which employs suction of a small quantity of air through airplane surfaces. This important technique offers the potential for significant reduction in drag and, thereby, for large increases in range or reductions in fuel usage for aircraft. For transport aircraft, the reductions in fuel consumed as a result of laminar-flow control may equal 30 percent of present consumption. Given such potential, it is obvious that active laminar-flow control with suction is an important technology. In this study, the author covers the early history of the subject and brings the story all the way to the mid-1990s with an emphasis on flight research, much of which occurred at Dryden.
Author : United States. Superintendent of Documents
Publisher :
Page : pages
File Size : 35,96 MB
Release : 1985
Category : Government publications
ISBN :
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
Author :
Publisher :
Page : 1508 pages
File Size : 39,89 MB
Release : 1991-03
Category : Government publications
ISBN :