An experimental and computational study was conducted to evaluate the performance and emissions characteristics of a candidate Lean Direct Injection (LDI) combustor configuration with a mix of simplex and airblast injectors. The National Combustion Code (NCC) was used to predict the experimentally measured EINOx emissions for test conditions representing low power, medium power, and high-power engine cycle conditions. Of the six cases modeled with the NCC using a reduced-kinetics finite-rate mechanism and lagrangian spray modeling, reasonable predictions of combustor exit temperature and EINOx were obtained at two high-power cycle conditions
An effort was undertaken to perform CFD analysis of fluid flow in Lean-Direct Injection (LDI) combus...
Increasing the pressure and temperature of the engines of new generation supersonic airliners increa...
A low-NOx emission combustor concept has been developed for NASA's Environmentally Responsible Aircr...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions.This...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions. Thi...
The low-emissions combustor development described is directed toward advanced high pressure aircraft...
An effort was undertaken to analyze the performance of a model Lean-Direct Injection (LDI) combustor...
This paper summarizes the development of lean direct injection (LDI) combustor technology at, or in ...
The low-emissions combustor development at the NASA Glenn Research Center is directed toward advance...
This paper presents experimental results for a low-NOxaero gas turbine combustor, in particular, a t...
The Lean Direct Injection (LDI) combustor is one of the low-emissions combustors with great potentia...
A computational effort was undertaken to analyze the details of fluid flow in Lean-Direct Injection ...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions. Thi...
Aviation gas-turbine combustion demands high efficiency, wide operability and minimal trace gas emis...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions. Thi...
An effort was undertaken to perform CFD analysis of fluid flow in Lean-Direct Injection (LDI) combus...
Increasing the pressure and temperature of the engines of new generation supersonic airliners increa...
A low-NOx emission combustor concept has been developed for NASA's Environmentally Responsible Aircr...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions.This...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions. Thi...
The low-emissions combustor development described is directed toward advanced high pressure aircraft...
An effort was undertaken to analyze the performance of a model Lean-Direct Injection (LDI) combustor...
This paper summarizes the development of lean direct injection (LDI) combustor technology at, or in ...
The low-emissions combustor development at the NASA Glenn Research Center is directed toward advance...
This paper presents experimental results for a low-NOxaero gas turbine combustor, in particular, a t...
The Lean Direct Injection (LDI) combustor is one of the low-emissions combustors with great potentia...
A computational effort was undertaken to analyze the details of fluid flow in Lean-Direct Injection ...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions. Thi...
Aviation gas-turbine combustion demands high efficiency, wide operability and minimal trace gas emis...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions. Thi...
An effort was undertaken to perform CFD analysis of fluid flow in Lean-Direct Injection (LDI) combus...
Increasing the pressure and temperature of the engines of new generation supersonic airliners increa...
A low-NOx emission combustor concept has been developed for NASA's Environmentally Responsible Aircr...