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Effect of liner air-entry holes, fuel state, and combustor size on performance of an annular turbojet combustor at low pressures and high air-flow rates

Effect of fuel injectors and liner design on performance of an annular turbojet combustor with vapor fuel

Performance of an annular turbojet combustor having reduced pressure losses and using propane fuel

Effect of Fuel Injectors and Liner Design on Performance of an Annular Turbojet Combustor With Vapor Fuel

Performance of a vaporizing annular turbojet combustor at simulated high altitudes

Preliminary investigation of an annular turbojet combustor having a catalytic-coated liner

Combustion performance of two experimental turbojet annular combustors at conditions simulating high-altitude supersonic flight

Combustion Performance of Two Experimental Turbojet Annular Combustors at Conditions Simulating High-Altitude Supersonic Flight

Performance of a short turbojet combustor with hydrogen fuel in a quarter-annulus duct and comparison with performance in a full-scale engine

Performance at simulated high altitudes of a prevaporizing annular turbojet combustor having low pressure loss

Performance at Simulated High Altitudes of a Prevaporizing Annular Turbojet Combustor Having Low Pressure Loss

Performance of a Short Turbojet Combustor With Hydrogen Fuel in a Quarter-Annulus Duct and Comparison With Performance in a Full-Scale Engine

Performance of an experimental annular turbojet combustor with methane and propane


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