Aircraft Vortex Wakes in Relation to Terminal Operations
Author : Joseph W. Wetmore
Publisher :
Page : 32 pages
File Size : 37,19 MB
Release : 1963
Category : Eddies
ISBN :
Author : Joseph W. Wetmore
Publisher :
Page : 32 pages
File Size : 37,19 MB
Release : 1963
Category : Eddies
ISBN :
Author : Joseph W. Wetmore
Publisher :
Page : 32 pages
File Size : 31,87 MB
Release : 1963
Category : Eddies
ISBN :
Author : Robert C. Nelson
Publisher :
Page : 144 pages
File Size : 49,57 MB
Release : 1974
Category : Aerodynamics
ISBN :
The investigation deals with the dynamic behavior of an airplane encountering aircraft wake turbulence. A digital computer simulation was developed to study the response of an aircraft flying into a trailing vortex wake. The simulation includes the complete six degree of freedom equations of motion, a description of the vortex velocity field, unsteady aerodynamics, and pilot control input. The parameters included the penetration angle, separation distance, aircraft size, and pilot control input. Predicted vortex induced motions are presented for general aviation, business, and light jet transport type aircraft.
Author :
Publisher :
Page : 798 pages
File Size : 28,75 MB
Release : 1972
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher :
Page : 1152 pages
File Size : 18,61 MB
Release : 1965
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 594 pages
File Size : 36,97 MB
Release : 1992
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 450 pages
File Size : 13,71 MB
Release :
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 92 pages
File Size : 27,35 MB
Release : 1963-07
Category : Government publications
ISBN :
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher :
Page : 258 pages
File Size : 39,6 MB
Release : 1963
Category : Aeronautics
ISBN :
Author : John Olsen
Publisher : Springer Science & Business Media
Page : 599 pages
File Size : 48,46 MB
Release : 2012-12-06
Category : Technology & Engineering
ISBN : 1468483463
The combination of increasing airport congestion and the ad vent of large transports has caused increased interest in aircraft wake turbulence. A quantitative understanding of the interaction between an aircraft and the vortex wake of a preceding aircraft is necessary for planning future high density air traffic patterns and control systems. The nature of the interaction depends on both the characteristics of the following aircraft and the characteristics of the wake. Some of the questions to be answered are: What deter mines the full characteristics of the vortex wake? What properties of the following aircraft are important? What is the role of pilot response? How are the wake characteristics related to the genera ting aircraft parameters? How does the wake disintegrate and where? Many of these questions were addressed at this first Aircraft Wake Turbulence Symposium sponsored by the Air Force Office of Sci entific Research and The Boeing Company. Workers engaged in aero dynamic research, airport operations, and instrument development came from several count ries to present their results and exchange information. The new results from the meeting provide a current picture of the state of the knowledge on vortex wakes and their interactions with other aircraft. Phenomena previously regarded as mere curiosities have emerged as important tools for understanding or controlling vortex wakes. The new types of instability occurring within the wake may one day be used for promoting early dis integration of the hazardous twin vortex structure.