Feasibility study of hydrogen-ammonia synergistic combustion in scramjets across broad Mach ranges. [PDF]
Song X +6 more
europepmc +1 more source
Combustor technology for future aircraft
The continuing improvement of aircraft gas turbine engine operating efficiencies involves increases in overall engine pressure ratio increases that will result in combustor inlet pressure and temperature increases, greater combustion temperature rises ...
Tacina, Robert R.
core
Using internal air injection for fuel mixing enhancement of annular hydrogen jet behind an inclined strut in a supersonic combustor: computational study. [PDF]
Bouazzi Y +7 more
europepmc +1 more source
Combustion Characteristics and Emissions of 99% Cracked Ammonia Blends in a Gas Turbine Representative Swirl. [PDF]
Alnaeli M +4 more
europepmc +1 more source
Solving characteristic parameters of heavy-duty gas turbines using parameter estimation method. [PDF]
Chi J, Wang C, He Y, Gou C, Wang Z.
europepmc +1 more source
Time Series and Spectral Analysis of Thermoacoustic Oscillations for Propane-Oxyfuel Combustion in a Swirl-Stabilized, Nonpremixed Combustor. [PDF]
Talal Q +4 more
europepmc +1 more source
Gas Flaring Is Likely Underestimated by Satellites due to Undetected Small Flares. [PDF]
Seymour SP +4 more
europepmc +1 more source
OH* Chemiluminescence Characteristics of the RP-3 Fueled Dual-Swirl Direct-Mixing Combustor. [PDF]
Feng X, Liang H, Suo J, Zheng L.
europepmc +1 more source
Enhancing NO<sub>x</sub> emission control and energy efficiency of H<sub>2</sub>/NH<sub>3</sub> powered micro generator in a planar porous combustor. [PDF]
Wang H +9 more
europepmc +1 more source

