Mixing of multiple dilution jets with a hot primary airstream for gas turbine combustors

Author:

HOLDEMAN J.1,WALKER R.2,KORS D.2

Affiliation:

1. NASA, Lewis Research Center, Cleveland, Ohio

2. Aerojet Liquid Rocket Co., Sacramento, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Reference6 articles.

1. Profiles in the Plane of Symmetry Domatraam of a Jet Injected Normal to a Crossflow." TN 0-6966, Sept. 1972, NASA. 4. Walker, R. E. and Kors. D. L. 't-fultipleJet

2. Jet Mixing Study for Gas Turbine Combustors," TN D-4695, Aug. 1968, NASA.

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1. Experimental and Numerical Study on the Effect of Annular Combustor Design on Thermal Uniformity Jet in Crossflow;Journal of Energy Resources Technology;2022-04-01

2. Turbulent fuel-air mixing study of jet in crossflow at different velocity ratios using LES;International Journal of Heat and Fluid Flow;2020-10

3. Unsteady behaviour of opposite impinging jets interaction in crossflow;Transactions of the JSME (in Japanese);2017

4. Effect of Cross-flow Momentum on Opposing Jet Mixing;International Journal of Gas Turbine, Propulsion and Power Systems;2014

5. Numerical and Experimental Study of the Effect of Momentum-Flux Ratio on Temperature Uniformity in the Combustor;11th International Energy Conversion Engineering Conference;2013-07-12

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