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contributor authorM. R. Nalim
contributor authorD. E. Paxson
date accessioned2017-05-08T23:53:25Z
date available2017-05-08T23:53:25Z
date copyrightJuly, 1997
date issued1997
identifier issn1528-8919
identifier otherJETPEZ-26766#668_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118665
description abstractWave rotor cycles that utilize premixed combustion processes within the passages are examined numerically using a one-dimensional CFD-based simulation. Internal-combustion wave rotors are envisioned for use as pressure-gain combustors in gas turbine engines. The simulation methodology is described, including a presentation of the assumed governing equations for the flow and reaction in the channels, the numerical integration method used, and the modeling of external components such as recirculation ducts. A number of cycle simulations are then presented that illustrate both turbulent-deflagration and detonation modes of combustion. Estimates of performance and rotor wall temperatures for the various cycles are made, and the advantages and disadvantages of each are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Numerical Investigation of Premixed Combustion in Wave Rotors
typeJournal Paper
journal volume119
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2817036
journal fristpage668
journal lastpage675
identifier eissn0742-4795
keywordsCombustion
keywordsWaves
keywordsRotors
keywordsCycles
keywordsExplosions
keywordsTurbulence
keywordsDucts
keywordsEquations
keywordsWall temperature
keywordsCombustion chambers
keywordsComputational fluid dynamics
keywordsEngineering simulation
keywordsGas turbines
keywordsModeling
keywordsChannels (Hydraulic engineering)
keywordsPressure AND Flow (Dynamics)
treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 003
contenttypeFulltext


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