Ground Vortex Workshop
Author : Richard J. Margason
Publisher :
Page : 224 pages
File Size : 19,25 MB
Release : 1988
Category : Ground-cushion phenomenon
ISBN :
Author : Richard J. Margason
Publisher :
Page : 224 pages
File Size : 19,25 MB
Release : 1988
Category : Ground-cushion phenomenon
ISBN :
Author :
Publisher :
Page : 1070 pages
File Size : 46,86 MB
Release : 1974
Category :
ISBN :
Author :
Publisher :
Page : 36 pages
File Size : 45,61 MB
Release : 1982
Category : Aeronautics
ISBN :
The naval aviation safety review.
Author : Dale N. Jones
Publisher :
Page : 38 pages
File Size : 12,25 MB
Release : 1970
Category : Atmospheric turbulence
ISBN :
Author : Reiner Decher
Publisher : Springer Nature
Page : 178 pages
File Size : 48,82 MB
Release : 2022-02-25
Category : Technology & Engineering
ISBN : 9811680280
This open access book is an introduction for the lay reader to understand the basics of flight. The exposure is to the mysteries of lift generation by wings and the basic function of the jet propulsion engine. The text relies on simple descriptions of the physics of air flow without unduly involving mathematics. The text is richly illustrated with sketches and photographs to enrich verbal descriptions. The book takes the viewpoint that a reader does not have a background in the engineering of airplane components but is interested in the subject. The description is in terms of easy-to-understand terminology, occasional use of humor, references to everyday experiences, and occasionally to an algebraic relationship when that is unavoidable. This book would serve a student aspiring to be an engineer to begin grappling with the phenomena involved and the techniques used to analyze these phenomena. The practitioner, as well as the beginner, in the art of flying an airplane is well served with the knowledge exposed here. The text makes no apology for technical complexity. Its introduction is rigorous and provides a sound footing for further study.
Author : A.S. Ginevsky
Publisher : Springer Science & Business Media
Page : 166 pages
File Size : 25,90 MB
Release : 2009-07-07
Category : Mathematics
ISBN : 3642017606
Investigation of vortex wakes behind various aircraft, especially behind wide bodied and heavy cargo ones, is of both scientific and practical in terest. The vortex wakes shed from the wing’s trailing edge are long lived and attenuate only atdistances of10–12kmbehindthe wake generating aircraft. The encounter of other aircraft with the vortex wake of a heavy aircraft is open to catastrophic hazards. For example, air refueling is adangerous operationpartly due to thepossibility of the receiver aircraft’s encountering the trailing wake of the tanker aircraft. It is very important to know the behavior of vortex wakes of aircraft during theirtakeoff andlanding operations whenthe wakes canpropagate over the airport’s ground surface and be a serious hazard to other depart ing or arriving aircraft. This knowledge can help in enhancing safety of aircraft’s movements in the terminal areas of congested airports where the threat of vortex encounters limits passenger throughput. Theoreticalinvestigations of aircraft vortex wakes arebeingintensively performedinthe major aviationnations.Usedforthispurpose are various methods for mathematical modeling of turbulent flows: direct numerical simulation based on the Navier–Stokes equations, large eddy simulation using the Navier–Stokes equations in combination with subrigid scale modeling, simulation based on the Reynolds equations closed with a differential turbulence model. These approaches are widely used in works of Russian and other countries’ scientists. It should be emphasized that the experiments in wind tunnels and studies of natural vortex wakes behind heavy and light aircraft in flight experiments are equally important.
Author : Robert C. Costen
Publisher :
Page : 76 pages
File Size : 23,56 MB
Release : 1970
Category : Winds
ISBN :
A new equation is derived for the motion of vorticity in a general fluid, including the effects of viscosity, compressibility, nonhomogeneity, and nonconservative forces. The equation holds, in particular, for vortices which may not move with the fluid. A linearized form of this equation is applied to tornado cyclones and to the twin tornado of April 11, 1965, near Elkhart, Indiana. It is shown that the displacement of tornado cyclones to the right of the mean tropospheric winds may be accounted for by the upward efflux of fluid from the cyclone into the jet stream. Also, the retarded revolution rate of the twin tornado may be due in part to an attractive "buoyancy" force acting on the partially rarefied cores of the pair.
Author :
Publisher :
Page : 296 pages
File Size : 31,82 MB
Release : 1991
Category : Aeronautics
ISBN :
Author : Kyoji Kamemoto
Publisher : World Scientific
Page : 228 pages
File Size : 11,49 MB
Release : 2000-05-11
Category : Technology & Engineering
ISBN : 9814493287
Vortex methods have been developed and applied to many kinds of flows related to various problems in wide engineering and scientific fields. The purpose of the First International conference on Vortex methods was to provide an opportunity for engineers and scientists to present their achievements, exchange ideas and discuss new developments in mathematical and physical modeling techniques and engineering applications of vortex methods.
Author : United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation
Publisher :
Page : 298 pages
File Size : 17,17 MB
Release : 1995
Category : Science
ISBN :
Distributed to some depository libraries in microfiche.