Aviation kerosene is commonly used in combustion and regenerative engine cooling
processes in propulsion and power-generation systems, including rocket, scramjet, and …

A flue gas internal and external double cycle low nitrogen burner was established. Using the
method of orthogonal test, the number (n), inclination angle (i) and diameter (d) of the …

In this work, a three-staged multi-injection based on the triple-swirler technique was
proposed and investigated, which can broaden the engine envelope than a two-staged fuel …

There is a need for fast and reliable emissions prediction tools in the design, development
and performance analysis of gas turbine combustion systems to predict emissions such as …

Many sources of uncertainty exist when emissions are modeled for a gas turbine combustion
system. They originate from uncertain inputs, boundary conditions, calibration, or lack of …

Direct thermal imprinting of nanostructures on glass substrates is reliable when
manufacturing net-shaped glass devices with various surface functions. However, several …

The present paper describes the design of a toroidal jet-stirred reactor (TJSR) for lean
blowoff and emissions studies of ammonia-hydrogen mixtures at atmospheric pressure, with …

An increasingly common experimental method allows determination of the overall
effectiveness of a film cooled turbine component. This method requires the Biot number of …

Aviation NOₓ emissions are a significant factor in causing air quality deterioration, leading
to potentially 16,000 annual premature deaths globally. To cope with the expected increase …

Numerical optimization of nitrogen oxides (NOx) formation is an essential factor during
developing low pollution combustor of gas turbine. The Computational Fluid Dynamics …