Aeroacoustic Measurements of a Scaled Half-Model at High Reynolds Numbers
Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge
Analysis of Conformable Pressure Vessels: Introducing the Multi-Bubble
Application of Resonant Femtosecond Tagging Velocimetry in the 0.3-Meter Transonic Cryogenic Tunnel
Architecture for Lunar Return Using Existing Assets
Assessment of Electric-Pump-Fed Nuclear Thermal Propulsion for Near-Term Missions
Base-Pressure Experimental Investigation on a Space Launcher in Subsonic Regime
Cavitation Instabilities During the Development Testing of a Liquid Oxygen Pump
CFD Modeling of Bidirectional PMDs Inside Cryogenic Propellant Tanks Onboard Parabolic Flights
Characteristics of Thermal Cavitation on a Two-Dimensional Hydrofoil
Characterization of Flashing Phenomena with Cryogenic Fluid Under Vacuum Conditions
Characterizing High-Energy-Density Propellants for Space Propulsion Applications
Comprehensive Study of Cryogenic Fluid Dynamics of Swirl Injectors at Supercritical Conditions
Computational Fluid Dynamics Analysis of Jet-Ullage Interactions During Microgravity Mixing
Coupling of Cryogenic Oxygen–Hydrogen Flames to Longitudinal and Transverse Acoustic Instabilities
Current Status of Liquid-Bipropellant Detonation-Based Propulsion Devices
Design Considerations for an Earth–Mars Cycler Spacecraft Using the S1L1 Cycler
Difficulties in Dual-Mode Operation of Nontoxic Hypergolic Thruster Using Decomposition of
Durability and Survivability of Piezoelectric Wafer Active Sensors on Metallic Structure
Dynamical Chilldown Model of a Liquid Hydrogen Feed System
Effect of Injector Design on the Combustion of Ethanol and Hydrogen-Peroxide Sprays
Effect of Isogrid-Type Obstructions on Thermal Stratification in Upper-Stage Rocket Propellant Tanks
Effect of Return Inlet on Thermal Stratification in a Rocket Tank
Effects of Injector Geometry on Cryogenic Shear Coaxial Jets at Supercritical Pressures
Effects of Wall-Injection Length on Spray and Combustion in a Coaxial Porous Injector
Electric Feed Systems for Liquid-Propellant Rockets
Estimation of Thin-Film Contribution in Phase Change Calculations Involving Cryogenic Propellants
Evaluation of Cryogenic Force Balance Calibration Methodologies Relative to Wind Tunnel Results
Experimental Investigation of Heat Transfer in a Subscale Liquid Rocket Engine
Experimental Investigation of Methane Convection and Boiling in Rocket Engine Cooling Channels
Experimental Investigation of Spherical Tank Slosh Dynamics with Water and Liquid Nitrogen
Explosion Hazard from a Propellant-Tank Breach in Liquid Hydrogen-Oxygen Rockets
Extension of a Standard Flow Solver for Simulating Phase Change in Cryogenic Tanks
Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Transonic, Cryogenic Wind Tunnel
Fragment Acceleration Modeling for Pressurized Tank Burst
Gas Permeability and Flexural Strength of Impacted Composites for Cryogenic Propellant Tanks
Gas Permeation of Composites Subjected to Impact for Cryogenic Applications
Geometrical Installation and Deformation Effects in High-Lift Flows
Heat Transfer in Rocket Combustion Chambers Firing Plates: Role of Injector Confinement
Highly Elliptical Rendezvous Orbits to Minimize Cryogenic Propellant Losses and Maximize Payload
Homogeneous Equilibrium Modeling for Subcritical Flows in Liquid Rocket Engine Cooling Systems
Hybrid Continuum/Rarefied Flow Simulations of Plume Interaction with Full-Sized Spacecraft
Identification of Flap Side-Edge Two-Source Mechanism Based on Phased Arrays
Impact Identification in Sandwich Structures Using Solitary Wave-Supporting Granular Crystal Sensors
Impedance- and Lamb-Waves-Based Health Condition Monitoring Approach for Composite Cryotanks
Influence of Contact Angle and Tube Size on Capillary-Driven Flow Under Microgravity