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