Determination of Captive Flight Loads and Separation Trajectories of Airborne Stores
Author : Dale E. Knutsen
Publisher :
Page : 72 pages
File Size : 12,80 MB
Release : 1968
Category : Airplanes
ISBN :
Author : Dale E. Knutsen
Publisher :
Page : 72 pages
File Size : 12,80 MB
Release : 1968
Category : Airplanes
ISBN :
Author : Guy Saunders
Publisher :
Page : pages
File Size : 26,73 MB
Release : 1998
Category :
ISBN :
Author : David J. Fisk
Publisher :
Page : 88 pages
File Size : 13,72 MB
Release : 1992
Category : Radar
ISBN :
Author : A. R. Maddox
Publisher :
Page : 46 pages
File Size : 49,12 MB
Release : 1978
Category : Loads (Mechanics).
ISBN :
Author : Thomas J. Mueller
Publisher : Springer Science & Business Media
Page : 456 pages
File Size : 18,82 MB
Release : 2013-03-08
Category : Science
ISBN : 3642840108
Current interest in a variety of low Reynolds number applications has focused attention on the design and evaluation of efficient airfoil sections at chord Reynolds numbers from about 100,000 to about 1,000,000. These applications include remotely piloted vehicles (RPVs) at high altitudes, sailplanes, ultra-light man-carrying/man powered aircraft, mini-RPVs at low altitudes and wind turbines/propellers. The purpose of this conference was to bring together those researchers who have been active in areas closely related to this subject. All of the papers presented are research type papers. Main topics are: Airfoil Design and Analysis, Computational Studies, Stability and Transition, Laminar Separation Bubble, Steady and Unsteady Wind Tunnel Experiments and Flight Experiments.
Author :
Publisher :
Page : 906 pages
File Size : 32,12 MB
Release : 1960
Category : Aeronautics
ISBN :
Author : R. W. Butler
Publisher :
Page : 50 pages
File Size : 28,67 MB
Release : 1981
Category : Angle of attack (Aerodynamics)
ISBN :
A captive testing technique capable of simulating aircraft maneuvers at high angles of attack has been developed and tested in the Aerodynamic Tunnel 16T of the Arnold Engineering Development Center (AEDC). The captive technique uses a closed loop system between wind tunnel, model, and computer. Use of the wind tunnel as an analog forcing function eliminates the requirement for a conventional static data matrix in motion simulation. Various high angle-of-attack maneuvers (rudder roll, aileron roll, wind-up turn, etc.) were generated with the captive system and show good correlation with flight data. (Author).
Author :
Publisher :
Page : 0 pages
File Size : 47,1 MB
Release : 1968
Category :
ISBN :
A summary of the state-of-the-art in determining captive flight loads and separation trajectories of airborne stores is presented. The summary is based largely on a recent survey of appropriate aerospace concerns and government installations. Responses to the survey indicate that the present state-of-the-art does not allow an accurate general analytical solution to the problem except under the most idealized situations. Testing of the specific aircraft/store combination is therefore recommended unless the combination closely matches a previously tested combination for which data are available. (Author).
Author : Susana Rotker
Publisher : U of Minnesota Press
Page : 264 pages
File Size : 23,82 MB
Release : 2002
Category : Argentina
ISBN : 9781452905921
Author :
Publisher :
Page : 940 pages
File Size : 36,62 MB
Release : 1977
Category : Aeronautics
ISBN :