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WASSERSTOFF
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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
Element Potential-Based Procedure for Metamodeling of Combustion Products
Enhanced Supersonic Combustion Targeting Combustor Length Reduction in a Mach 12 Scramjet