Evaluation of Flip-Flop Jet Nozzles for Use as Practical Excitation Devices

Author:

Raman Ganesh1,Rice Edward J.2,Cornelius David M.3

Affiliation:

1. NYMA, Inc., NASA Lewis Research Center Group, Brookpark, OH 44142

2. NASA Lewis Research Center, Cleveland, OH 44135

3. Department of Aeronautics and Astronautics, Stanford University, Stanford, CA 94305

Abstract

This paper describes the flowfield characteristics of the flip-flop jet nozzle and the potential for using this nozzle as a practical excitation device. It appears from the existing body of published information that there is a lack of data on the parameters affecting the operation of such nozzles and on the mechanism of operation of these nozzles. An attempt is made in the present work to study the important parameters affecting the operation and performance of a flip-flop jet nozzle. Measurements were carried out to systematically assess the effect of varying the nozzle pressure ratio (NPR) as well as the length and volume of the feedback tube on the frequency of oscillation of this device. Flow visualization was used to obtain a better understanding of the jet flowfield and of the processes occurring within the feedback tube. The frequency of oscillation of the flip-flop jet depended significantly on the feedback tube length and volume as well as on the nozzle pressure ratio. In contrast, the coherent velocity perturbation levels did not depend on the above-mentioned parameters. The data presented in this paper would be useful for modeling such flip-flop excitation devices that are potentially useful for controlling practical shear flows.

Publisher

ASME International

Subject

Mechanical Engineering

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