Ground-based measurements of the wake vortex characteristics of a B747 aircraft in various configurationsA Boeing 747 aircraft flew 54 passes at low level over ground-based sensors. Vortex velocities were measured by a laser-Doppler velocimeter, an array of monostatic acoustic sounders, and an array of propeller anemometers. Flow visualization of the wake was achieved using smoke and balloon tracers. Preliminary results were obtained on the initial downwash field, the time for merging of the multiple vortices, the velocity fields, vortex decay, and the effects of spoilers and differential flap settings on the dissipation and structure of vortices.
Document ID
19770036918
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hallock, J. N. (AeroVironment, Inc. Pasadena, CA, United States)
Burnham, D. C. (U.S. Department of Transportation, Transportation Systems Center Cambridge, Mass., United States)
Tombach, I. H. (AeroVironment, Inc. Pasadena, Calif., United States)
Brashears, M. R. (AeroVironment, Inc. Pasadena, CA, United States)
Zalay, A. D. (Lockheed Missiles and Space Co., Inc. Huntsville, Ala., United States)
Barber, M. R. (NASA Flight Research Center Edwards, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 77-9Report Number: AIAA PAPER 77-9
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Los Angeles, CA
Start Date: January 24, 1977
End Date: January 26, 1977
Sponsors: American Institute of Aeronautics and Astronautics