Hot fire tests were performed using a single-injector research combustor featuring a large
optical access window (255× 38 mm) for flame visualisation. Three test campaigns were …

Hot fire tests of a multi-injector research combustor were performed with liquid-oxygen and
liquefied-natural-gas (LOX/LNG) propellants at chamber pressures from 30 up to 67 bar …

The rotating detonation combustor is investigated as a potential implementation of pressure-
gain combustion. Achieving net pressure-gain has proven to be extremely challenging in …

This Special Issue, entitled “The Design and Optimization of Fire Protection Processes”, has
been created to help readers gain new insights into the field of fire protection. The world's …

An experimental study was conducted to visualize the dynamics and spectra of single-
element shear coaxial liquid oxygen (LOX)/gaseous methane flames at high but still …

The maximum attainable thermal efficiency of conventional rocket combustion devices is
limited by the ideal Brayton-Joule thermodynamic cycle. The Brayton-Joule cycle is …

Hot fire tests were performed with a single-injector research combustor featuring a large
optical access window (255x38 mm) for flame visualisation. Three test campaigns were …

View Video Presentation: https://doi. org/10.2514/6.2023-1838. vid Flame radiation and
acoustic measurements were performed in a single-element, liquidoxygen/compressed-and …

A shear-coaxial-element is a prominent choice in terms of injection technology for
bipropellants with a high density ratio. While this type of injector performed well for liquid …

This study presents the design methodology and results from initial testing of an
experimental hydrogen-oxygen rotating detonation combustor (RDC). A small-scale heat …