Temperature and Gas Composition Analysis in Can-Type Gas Turbine Combustors with Different Fuel Injection Nozzles : Series B : Fluid Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties

スポンサーリンク

概要

• 論文の詳細を見る
• 一般社団法人日本機械学会の論文

著者

• YAMADA Hideshi

  National Aerospace Laboratory

• KUYAMA Tosiyuki

  Kawasaki Heavy Industry

• Miyagi Kohji

  Maruwa Electric

• TAMARU Taku

  National Aerospace Laboratory

関連論文

• On-Engine Testing of a Variable Geometry Lean-Premixed Combustor
• An Experimental Investigation on the Maximum Loading of a Practial Gas Turbine Combustor : Series B : Fluid Engineering, Heat Transfer, Combustion, Power, Thermophysical, Properties
• Temperature and Gas Composition Analysis in Can-Type Gas Turbine Combustors with Different Fuel Injection Nozzles : Series B : Fluid Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties
• TS-65 Application of Short-Flame/Quick-Quench Combustion Concept to Ultra-Low NO_x Gas Turbine Combustors(Session C-6 NO_x Reduction 1)

スポンサーリンク