Turbulence measurements in subsonic and supersonic axisymmetric jets in a moving streamMeasurements of mean and fluctuating velocity components are made in an unheated axisymmetric jet mounted in a low speed wind tunnel. The measurements are made with a backscatter laser velocimeter. Velocity measurements are presented for jet exit Mach numbers in the range .47 to 1.67 and tunnel velocity to jet exit velocity ratios in the range .1 to .5. The effects of velocity ratio and jet exit Mach number on the jet spreading and the turbulence levels are examined. The mean velocity, turbulence intensity, and axial velocity skewness and kurtosis are shown to agree with jets into still air measurements using an appropriate local radial coordinate based on the vorticity thickness.
Document ID
19760037955
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Morris, P. J. (Lockheed-Georgia Co. Marietta, Ga., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 76-25Report Number: AIAA PAPER 76-25
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 26, 1976
End Date: January 28, 1976
Sponsors: American Institute of Aeronautics and Astronautics