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