Lip noise generated by flow separation from nozzle surfacesFlow separation from nozzle surfaces can be a source of significant noise in addition to the jet noise. When no flow separation region exists only jet noise is observed at every angle, for velocities down to 120 m/sec, with both low and high levels of initial turbulence. Intense nearly periodic turbulence and noise is caused by flow separation from the thin core nozzle lip of a coaxial nozzle. This can be described by a combination of aeolian tone and trailing edge noise theory. Noise caused by flow separation from the surfaces of other nozzle geometries has somewhat different characteristics.
Document ID
19760037950
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Olsen, W. (NASA Lewis Research Center Cleveland, OH, United States)
Karchmer, A. (NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 76-3Report Number: AIAA PAPER 76-3
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