Wedge-Induced Oblique Detonations with Small Heat Release
Wave intersection limits for focused compression of air in chemical equilibrium
Water Electrolysis for Propulsion of a Crewed Mars Mission
Wall-Modeled Large-Eddy Simulation of Autoignition-Dominated Supersonic Combustion
Simulations of combustion in high-speed and supersonic flows need to account for autoignition phenomena, compressibility, and the
...Visualization of Pulse Firing Mode in Hypergolic Bipropellant Thruster
The pulse firing mode of bipropellant thrusters is crucial for the precise attitude control of spacecraft. This research explains how to
...Visualization of Coolant Liquid Film Dynamics in Hypergolic Bipropellant Thruster
We conduct a high-speed visualization of coolant liquid film dynamics inside a 10N-class bipropellant thruster using monomethylhydrazine
...Viscosity correlation for para-hydrogen in the gaseous and liquid states.
Velocity defect laws for transpired turbulent boundary layers
Validation of Pulse-Detonation Operation in Low-Ambient-Pressure Environment
Utilization and Loss of Available Energy for Chemical Rockets in Atmospheric Flight
Unsteady Simulations of Rocket Plume Expansions in Geostationary Earth Orbit
Unsteady, direct simulation Monte Carlo/particle-in-cell simulations of rocket plume expansions into the magnetosphere at geostationary
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Unmanned planetary spacecraft chemical rocket propulsion.
Unified Approach for Meso-Informed Burn Models in Shocked Energetic Materials
Two-Dimensional Model for Liquid-Rocket Transverse Combustion Instability
TURBULENCE EFFECTS IN CHEMICAL REACTION KINETICS MEASUREMENTS
Transmission Loss of Spacecraft Optical Materials Due to Ultraviolet-Induced Contamination
Transition Between Different Initiation Structures of Wedge-Induced Oblique Detonations