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Pressure and velocity measurements in a three dimensional wall jetIn three recent papers, some results of an experimental investigation of a freely expanding coflowing jet as well as a three dimensional wall jet have been presented. A flat plate as well as a curved wall surface intended to model a wing-flap combination in a high lift V/STOL configuration have been investigated. In these papers, the ratio of the jet exit plane velocity to the free stream velocity, was 5.1. This paper explores the effects of increasing the velocity ratio. The quantities measured include the width of the mixing region, the mean velocity field, turbulent intensities and time scales. In addition, wall and static pressure-velocity correlations and coherences are presented. The velocity measurements are made using a laser Doppler velocimeter with a phase-locked loop processor. The fluctuating pressures are monitored using condenser-type microphones.
Document ID
19790035670
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Catalano, G. D.
(USAF, Flight Dynamics Laboratory, Wright-Patterson AFB Ohio, United States)
Morton, J. B.
(Air Force Flight Dynamics Lab. Wright-Patterson AFB, OH, United States)
Humphris, R. R.
(Virginia, University Charlottesville, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 79-0352
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: New Orleans, LA
Start Date: January 15, 1979
End Date: January 17, 1979
Sponsors: Astronautics, American Institute of Aeronautics
Accession Number
79A19683
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-219
CONTRACT_GRANT: NSF 7522488
Distribution Limits
Public
Copyright
Other

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