Flow Behavior With an Oscillating Motion of the Impinging Jet in a Dump Diffuser Combustor

Author:

Honami S.1,Shizawa T.1,Sato A.2,Ogata H.3

Affiliation:

1. Department of Mechanical Engineering, Science University of Tokyo, Tokyo, 162, Japan

2. Aero-Engine and Space Operations, Ishikawajima-Harima, Heavy Industries Co., Ltd., Tokyo, Japan

3. Jet Engine Division, Kawasaki Heavy Industries Ltd., Kobe, Japan

Abstract

This paper presents flow behavior with an oscillating motion of an impinging jet upon a flame dome head and its reattachment to the casing wall, when a distorted flow is provided at the inlet of the dump diffuser combustor. A Laser-Doppler Velocimeter was used for the measurements of the time-averaged flow within a sudden expansion region. A surface pressure fluctuation survey on the flame dome head and flow visualization by a smoke wire technique with a high-speed video camera were conducted from the viewpoint of the unsteady flow features of the impinging jet. There exists a high-vorticity region at the jet boundary, resulting in the production of turbulence kinetic energy. In particular, higher vorticity is observed in the higher velocity side of the jet. The jet near the dome head has favorable characteristics about the flow rate distribution into the branched channel. Reynolds shear stress and turbulence energy are produced near the reattachment region. The jet has an oscillating motion near the dome head with asymmetric vortex formation at the jet boundary.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference6 articles.

1. Biaglow, J. A., 1971, “Effect of Various Diffuser Designs of the Performance on an Experimental Turbojet Combustor Insensitive to Radial Distortion of Inlet Airflow,” NASA TM X-2216.

2. Fishenden, C. R., and Stevens, S. J., 1974, “The Performance of Annular Combustor-Dump Diffusers,” AIAA Paper No. 74-1097.

3. Honami, S., and Morioka, T., 1990, “Flow Behavior in a Dump Diffuser With Distorted Flow at the Inlet,” ASME Paper No. 90-GT-90.

4. Klein, A., et al., 1974, “Experimental Investigation of the Performance of Short Annular Combustor-Dump Diffusers,” Proceedings, 2nd International Symposium on Air Breathing Engines, pp. 1–13.

5. Klein A. , et al., 1980, “The Effect of Blade-Wakes on the Performance of Short Dump-Diffuser Type Combustor Inlet,” ASME Journal of Fluids Engineering, Vol. 102, pp. 236–241.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Optimization Study of the Dump Diffuser in Gas Turbine to Reduce Pressure Loss;International Journal of Aerospace Engineering;2018-07-18

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