50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition : Development of the GE Aviation
TAPS II Public Final
GE Aviation Ramping Up Production for LEAP Engines | American Machinist
CLEEN III Supersonic Technology
Comparison of NO x emissions between the lean TAPS and a RQL combustor... | Download Scientific Diagram
Bjorn's Corner: Turbofan engine challenges, Part 5 - Leeham News and Analysis
Lean Combustion by Muliscale/Fractal Generated Turbulence in Gas Turbine Engines
TAPS II Public Final
LEAP – Lowering emissions - YouTube
The quantitative characterization of the ignition process for a lean staged injector: Influence of the air split between pilot swirlers - Jinhu Yang, Cunxi Liu, Fuqiang Liu, Yong Mu, Gang Xu, 2020
N+2 Advanced Low NOx Combustor Technology Final Report
General Electric Passport - Wikipedia
N+2 Advanced Low NOx Combustor Technology Final Report
CFM56 TAPS combustor - YouTube
TAPS II Public Final
Low Emission Commercial Aircraft Engine Combustor Development in China:From Airworthiness Requirements to Combustor Design
Low-Emissions Gas Turbine Combustion: Design Trends and Challenges
Low Emissions Propulsion Engine Combustor Technology Evolution Past, Present and Future
Synopsis of Propulsion Engine Combustion Technology/Product Development and Analysis Substantiated During Last 47 Years | SpringerLink
turbine - What is the difference between single and dual annular combustor? - Aviation Stack Exchange
Environmental Colloquium
Low Emissions Propulsion Engine Combustor Technology Evolution Past, Present and Future
A Triple-Flame, n+3 Generation Mixer
TAPS II Public Final
Experimental and numerical studies of a lean-burn internally-staged combustor - ScienceDirect
Bjorn's Corner: Turbofan engine challenges, Part 5 - Leeham News and Analysis
