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hydrogen
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keywords:(hydrogen)
Effects of Dilution and Pressure on Detonation Propagation Across an Inert Layer
Acoustic Waves Generated in Hypergolic Drop Tests of Low- and High-Volatility Fuels
Novel Hypergolic Green Fuels with Hydrogen Peroxide for Propulsion Systems
Temperature Distribution Within an Ignition Kernel Initiated by a Laser-Induced Plasma
Hybrid Systems Based on Solid Oxide Fuel Cells: Modelling and Design
Blended Wing Body Configuration for Hydrogen-Powered Aviation
Dual-Plate Injector for Throttling of Hydrogen Peroxide Monopropellant Thruster
Experimental Investigation of Decomposition with Cylindrical Pellets Catalyst
Exploiting Active Subspaces for Geometric Optimization of Cavity-Stabilized Supersonic Flames
Coherent Anti-Stokes Raman Spectroscopy of a Hydrogen Diffusion Flame in a Ramjet
Evaluation of Ethanol-Blended Hydrogen Peroxide Monopropellant on a 10 N Class Thruster
Diode Laser Absorption Sensor for Combustion Progress in a Model Scramjet
Scramjet Performance Computed for a JP-7-Fueled Generic X-51 Vehicle
Confined Boundary-Layer Flashback Flame Dynamics in a Turbulent Swirling Flow
Thermal Design and Experimental Verification of a Three-Dimensional-Printed Resistojet
Minimum-Fuel Ascent of a Hypersonic Vehicle Using Surrogate Optimization
Efficient Design Methods for Variable-Angle-Tow Composite Toroidal Pressure Vessels
Heat Transfer Operability Limits for an Actively and Passively Cooled Hypersonic Vehicle
Experimental Testing of an Airframe-Integrated Three-Dimensional Scramjet at Mach 10
Detonation-Driven Fuel-Injection System for Supersonic Combustion Testing Facilities
Supersonic Combustion of a Scramjet Engine Using Hydrogen Fuel in Shock Tunnel
Hydrogen Fuel Cells and Batteries for Electric-Vertical Takeoff and Landing Aircraft
Enhanced Supersonic Combustion Targeting Combustor Length Reduction in a Mach 12 Scramjet
Combustion of High-Pressure Hydrogen Diluted Mixtures in ESTHER Shock Tube
Convective and Radiative Wall Heat Transfer in Liquid Rocket Thrust Chambers
Critical Decay Time Model for Direct Detonation Initiation Energy in Gaseous Mixtures
Attaining Hypersonic Flight with Aluminum-Based Fuel-Rich Propellant
Low-Order Autoignition Modeling for Hydrogen Transverse Jets
Mode Change Characteristics of a Three-Dimensional Scramjet at Mach 8
Self-Adaptive Turbulence Eddy Simulation of Supersonic Combustor Considering Thermal Radiation
Comparison of Mach 10 Scramjet Measurements from Different Impulse Facilities
Optimization of Active and Passive Thermal Protection Systems for a Hypersonic Vehicle
Combined Cycle Nuclear System Architecture for Crewed Mars Spacecraft Propulsion and Power
Porous Versus Porthole Fuel Injection in a Radical Farming Scramjet: Numerical Analysis
Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet
Chemical Reaction Effects on Heat Loads of CH4/O2 and H2/O2 Rockets
Supersonic Boundary-Layer Combustion via Multiporthole Injector Arrays
Analytical Modeling of Heat Deposition in Propellant for Nuclear Thermal Rockets
Element Potential-Based Procedure for Metamodeling of Combustion Products