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Three component velocity measurements in an upper surface blowing configurationIn four recent papers, 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 and a curved wall surface modelling a wing-flap combination in a high lift V/STOL configuration have been documented as to their effects on the flow field. The ratio of the jet exit plane velocity to the free stream velocity was varied from 5.1 to 10.9 to 1. This report continues the documentation of the three dimensional wall jet with special emphasis on the vertical and lateral mean and fluctuating velocities. Additionally, boundary layer profiles over both the flat plate and the flap are presented.
Document ID
19790063903
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
August 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 79-1858
Report Number: AIAA PAPER 79-1858
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aircraft Systems and Technology Meeting
Location: New York, NY
Start Date: August 20, 1979
End Date: August 22, 1979
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
79A47916
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-219-3
CONTRACT_GRANT: NSF 75-22488
Distribution Limits
Public
Copyright
Other

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