Cavitation Instabilities During the Development Testing of a Liquid Oxygen Pump
Cavitation Instabilities During the Development Testing of a Liquid Oxygen Pump
Numerical Simulations of Internal Flow in an Aircraft Engine Pressure Swirl Atomizer
Numerical Simulations of Internal Flow in an Aircraft Engine Pressure Swirl Atomizer
Flow and Performance Analysis of Annular Cluster Truncated Plug Nozzle
Flow and Performance Analysis of Annular Cluster Truncated Plug Nozzle
Axisymmetric Jet Subjected to Radial and Azimuthal Forcing
Reduction of Aerodynamic Forcing Through Introduction of Stator Asymmetry in Axial Compressors
Modeling Vertical-Axis Wind-Turbine Performance: Blade-Element Method Versus Finite Volume Approach
Effect of Magnesium-Rich Phase on Oxidation Properties of Atomized Aluminum–Magnesium Powders
Beam-Riding Flight of a Laser Propulsion Vehicle Using Actively Controlled Pulse
Beam-Riding Flight of a Laser Propulsion Vehicle Using Actively Controlled Pulse
Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets
Potential of Variable-Geometry Method for Compressor Range Extension for Turbocharged Engines
Front Cellular Structure and Thrust Performance on Hydrogen–Oxygen Rotating Detonation Engine
Front Cellular Structure and Thrust Performance on Hydrogen–Oxygen Rotating Detonation Engine
Disturbance-Field Decomposition in a Transversely Forced Swirl Flow and Flame
Disturbance-Field Decomposition in a Transversely Forced Swirl Flow and Flame
The Rayleigh Efficiency of Pressure Gain Combustors
The Rayleigh Efficiency of Pressure Gain Combustors
Flow Characterization for a Shallow Single Serpentine Nozzle with Aft Deck
Flow Characterization for a Shallow Single Serpentine Nozzle with Aft Deck
Thrust Control by Fluidic Injection in Solid Rocket Motors
Thrust Control by Fluidic Injection in Solid Rocket Motors
High-Fidelity Simulations of Pressure-Gain Combustion Devices Based on Detonations
High-Fidelity Simulations of Pressure-Gain Combustion Devices Based on Detonations
Experimental and Numerical Performance Analysis of a Self-Starting Three-Dimensional Scramjet Intake
Boundary Layer Ingestion Propulsion Benefit for Transport Aircraft