A theoretical and experimental study of the impingement of two subsonic jets
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Authors
Gungor, Nihat
Subjects
Mixing of turbulent jet
Momentum exchange
Plane turbulent jet
Proportional amplifiers
Momentum exchange
Plane turbulent jet
Proportional amplifiers
Advisors
Sarpkaya, T.
Date of Issue
1969-06
Date
June 1969
Publisher
Monterey, California. U.S. Naval Postgraduate School
Language
en_US
Abstract
A theoretical and experimental investigation has been performed on the determination of the
characteristics of two impinging plane turbulent jets for the purpose of under1tanding the
performance of proportional fluid amplifiers and momentum-exchange devices . The jet deflection angle was determined through the application of the free-streamline theory for two normally impinging jets with arbitrary throat widths and wall set-backs . The deflection angle and the velocity and turbulence distributions acro1s and at various distances along the jet were determined through the use of a hot-wire anemometer system. The results are presented in terms of normalized parameters suitable for comparison with the theoretical predictions. The deflection angles predicted theoretically were found to be in good agreement with those obtained experimentally.
Type
Thesis
Description
Series/Report No
Department
Mechanical Engineering
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
Copyright is reserved by the copyright owner