Analysis of Nonplanar Wing-tip-mounted Lifting Surfaces on Low-speed Airplanes
Author : Cornelis P. Van Dam
Publisher :
Page : 180 pages
File Size : 28,72 MB
Release : 1983
Category : Aerodynamics
ISBN :
Author : Cornelis P. Van Dam
Publisher :
Page : 180 pages
File Size : 28,72 MB
Release : 1983
Category : Aerodynamics
ISBN :
Author : C. P. Van Dam
Publisher :
Page : 180 pages
File Size : 11,46 MB
Release : 1983
Category :
ISBN :
Author : Egbert Torenbeek
Publisher :
Page : 714 pages
File Size : 16,45 MB
Release : 2005
Category : Aerospace engineering
ISBN :
Author : National Research Council
Publisher : National Academies Press
Page : 77 pages
File Size : 30,93 MB
Release : 2007-08-06
Category : Technology & Engineering
ISBN : 030938382X
The high cost of aviation fuel has resulted in increased attention by Congress and the Air Force on improving military aircraft fuel efficiency. One action considered is modification of the aircraft's wingtip by installing, for example, winglets to reduce drag. While common on commercial aircraft, such modifications have been less so on military aircraft. In an attempt to encourage greater Air Force use in this area, Congress, in H. Rept. 109-452, directed the Air Force to provide a report examining the feasibility of modifying its aircraft with winglets. To assist in this effort, the Air Force asked the NRC to evaluate its aircraft inventory and identify those aircraft that may be good candidates for winglet modifications. This reportâ€"which considers other wingtip modifications in addition to wingletsâ€"presents a review of wingtip modifications; an examination of previous analyses and experience with such modifications; and an assessment of wingtip modifications for various Air Force aircraft and potential investment strategies.
Author :
Publisher :
Page : 1572 pages
File Size : 16,27 MB
Release : 1992
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 580 pages
File Size : 36,61 MB
Release : 1984
Category : Astronautics
ISBN :
Author :
Publisher :
Page : 1274 pages
File Size : 19,9 MB
Release : 1961
Category : Government publications
ISBN :
Author :
Publisher :
Page : 794 pages
File Size : 11,66 MB
Release : 1984
Category : Government publications
ISBN :
Author : C. P. Vandam
Publisher :
Page : 36 pages
File Size : 29,17 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 : 520 pages
File Size : 18,49 MB
Release : 1983-10
Category : Dissertations, Academic
ISBN :