Synonyme wurden verwendet für:
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
Diode Laser Absorption Sensor for Combustion Progress in a Model Scramjet
Evaluation of Ethanol-Blended Hydrogen Peroxide Monopropellant on a 10 N Class Thruster
Scramjet Performance Computed for a JP-7-Fueled Generic X-51 Vehicle
Confined Boundary-Layer Flashback Flame Dynamics in a Turbulent Swirling Flow
Minimum-Fuel Ascent of a Hypersonic Vehicle Using Surrogate Optimization
Heat Transfer Operability Limits for an Actively and Passively Cooled Hypersonic Vehicle
Thermal Design and Experimental Verification of a Three-Dimensional-Printed Resistojet
Hydrogen Fuel Cells and Batteries for Electric-Vertical Takeoff and Landing Aircraft
Detonation-Driven Fuel-Injection System for Supersonic Combustion Testing Facilities
Enhanced Supersonic Combustion Targeting Combustor Length Reduction in a Mach 12 Scramjet
Supersonic Combustion of a Scramjet Engine Using Hydrogen Fuel in Shock Tunnel
Experimental Testing of an Airframe-Integrated Three-Dimensional Scramjet at Mach 10
Convective and Radiative Wall Heat Transfer in Liquid Rocket Thrust Chambers
Low-Order Autoignition Modeling for Hydrogen Transverse Jets
Critical Decay Time Model for Direct Detonation Initiation Energy in Gaseous Mixtures
Attaining Hypersonic Flight with Aluminum-Based Fuel-Rich Propellant
Mode Change Characteristics of a Three-Dimensional Scramjet at Mach 8
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
Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet
Analytical Modeling of Heat Deposition in Propellant for Nuclear Thermal Rockets
Chemical Reaction Effects on Heat Loads of CH4/O2 and H2/O2 Rockets
Element Potential-Based Procedure for Metamodeling of Combustion Products
Porous Versus Porthole Fuel Injection in a Radical Farming Scramjet: Numerical Analysis
Supersonic Boundary-Layer Combustion via Multiporthole Injector Arrays
Hypervelocity Experiments on Oxygen Enrichment in a Hydrogen-Fueled Scramjet
Impact of Liquid-Hydrogen Fuel-Cell Electric Propulsion on Aircraft Configuration and Integration