combustor : Related Words Words similar in meaning to combustor
- combustion zone«
- fuel«
- liner«
- combustors«
- air«
- fuel injector«
- swirler«
- primary air«
- emission«
- afterburner«
- igniter«
- annular combustors«
- engine«
- type«
- combustion«
- ramjet combustors«
- cannular combustor«
- aircraft application«
- gas turbine engine«
- co«
- scramjet engine«
- diffuser«
- injector«
- liner hole«
- double annular combustor«
- dilution air«
- temperature«
- temperature profile«
- gas turbine«
- swirlers«
- turbine«
- casing«
- most modern engine«
- main combustor«
- combustion process«
- carbon monoxide«
- turbulence«
- dome«
- annular combustor«
- pressure«
- nitrogen oxide«
- smoke«
- nox«
- unburned hydrocarbon«
- combustion chamber«
- method«
- air mixture«
- uniform temperature profile«
- type combustors«
- liner cooling«
- emission section«
- dump combustors«
- combustor technology«
- air blast injector«
- separate combustion zone«
- intermediate air«
- exit flow«
- ramjet«
- cool air«
- uhcs«
- transpiration cooling«
- gas turbine combustors«
- pilot zone«
- slat«
- film cooling«
- co emission«
- nozzle«
- airflow«
- tube«
- compressor«
- turbine section«
- secondary air«
- turbine stage«
- annular«
- low power level«
- uhc«
- combustion air«
- flame«
- co2«
- cooling«
- scramjet«
- main zone«
- design challenge«
- mass flow«
- carbon dioxide«
- thrust«
- amount«
- residence time«
- transpiration«
- temperature rise«
- pressure vessel«
- disadvantage«
- annulus«
- dac«
- maximum power«
- efficiency«
- difference«
- dilution«
- hot spot«
- jet engine«
- pollutant«
- mach«
- major difference«
- velocity optimal«
- vaporizing fuel injector«
- vaporizer tube«
- uniform exit temperature profile«
- uniform exit temperature«
- uhc emission«
- uhc content«
- type combustor«
- turbine blade technology«
- traditional gas turbine combustors«
- system ignition«
- supersonic flow environment«
- successful emission reduction«
- standard annular combustor«
- smokeless combustors«
- small physical size«
- scramjets«
- scramjet combustors«
- reason liner«
- primary combustors«
- power generating gas turbine«
- porous liner«
- most modern gas turbine engine«
- most igniter«
- most combustors«
- modern gas turbine design«
- modern fuel injector«
- max reheat«
- max dry«
- main combustor counterpart«
- main combustion air«
- lowest pressure drop«
- lower fuel pressure«
- low co combustor«
- local low pressure zone«
- isolator section«
- hastelloy x.«
- fuel injector section«
- flameholders«
- electrical spark igniter«
- early gas turbine engine«
- early combustors«
- conventional combustors«
- combustor research«
- combustor exhaust«
- combustor durability«
- combustor advance«
- co emission result«
- cannular«
- bluff body dome«
- annular tubo«
- airblast fuel injector«
- snout«
- uneven profile«
- uneven combustion«
- traditional gas turbine engine«
- thin film cooling«
- size test rig«
- single annular combustor«
- scramjet combustor«
- ramjets«
- nozzle guide vane«
- military supersonic aircraft«
- maximum thrust wet«
- maximum thrust dry«
- main combustors«
- low fuel flow«
- jet pipe downstream«
- idle throttle«
- homogeneous droplet«
- discrete combustion zone«
- conventional gas turbine engine«
- automotive spark plug«
- air splitter«
- afterburners«
- durability«
- path«
- turbine(s«
- total airflow«
- secondary air flow«
- royce tay turbofan«
- gas turbine engine component«
- gas turbine application«
- continuous liner«
- assist technique«
- path section«
- fuel mixing«
- fuel concentration«
- separate liner«
- oxygen injection«
- low speed flow«
- low pressure loss«
- flow distortion«
- cylindrical combustion chamber«
- velocity result«
- most modern design«
- local pocket«
- flow effect«
- early jet engine«
- combustion heat«
- upstream«
- uniform combustion«
- supersonic aircraft design«
- limited concern«
- annular design«
- aircraft emission«
- afterburner section«
- advantage«
- unwanted emission«
- supersonic combustion ramjet«
- multiple can«
- common ring«
- shorter size«
- pressure flow«
- stable combustion«
- whitney jt8d«
- lower setting«
- can«
- velocity gas«
- rim-8 talos missile«
- lower pressure drop«
- engine setting«
- paths«
- flame holder«
- performance alloy«
- environmental emission«
- combustion section«
- unburnt hydrocarbon«
- benefit similar«
- simple plate«
- general electric j79«
- temperature cycle«
- bluff body«
- main configuration«
- air flow rate«
- unburnt fuel«
- boundary layer separation«
- turboshafts«
- thermal barrier coating«
- inlet air«
- continuous ring«
- air pass«
- afterburning«
- cfm international cfm56«
- extra thrust«
- combust«
- driving factor«
- compression system«
- fundamentals«
- testing«
- reaction process«
- inlet pressure«
- design factor«
- air blast«
- thermal load«
- set«
- thrust engine«
- superalloys«
- pressure compressor«
- transient response«
- operating characteristic«
- conventional type«
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