Performance of Choked Unsteady Ejector-Nozzles for use in Pressure Gain Combustors-Reference-Cited by-同舟云学术

Performance of Choked Unsteady Ejector-Nozzles for use in Pressure Gain Combustors

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Heffer Jonathan¹,Miller Robert¹

Affiliation:

1. Whittle Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1063

Reference6 articles.

1. A Simple Pressure-Gain Combustor for Gas Turbines

2. 5C.D.Porter.Valveless-gas-turbinecombustorswithpressuregain.ASMEPaperNo.58-GTP-11,pages179-184,1958. 6Lefebvre,Arthur,H.,GasTurbineCombustion,TaylorandFrancis,1999,Chapt.4. 7 Watson,N.andJanota,M.Turbochargingtheinternalcombustionengine.MacMillan1982 8MasonS.A.andMillerR.J.2006ThePerformanceofEjectorsDrivenbySinusoidallyUnsteadyJets.AIAA2006-1020

3. Heffer, Miller and Freeman, The time resolved flow within an ejector driven by a sinusoidally unsteady jet, AIAA 2008-117

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