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Theoretical Analysis of Dual-Thrust Rocket Motors with Intermediate Nozzle
Theoretical Analysis of Dual-Thrust Rocket Motors with Intermediate Nozzle
Front Cellular Structure and Thrust Performance on Hydrogen–Oxygen Rotating Detonation Engine
Front Cellular Structure and Thrust Performance on Hydrogen–Oxygen Rotating Detonation Engine
Experimental and Numerical Performance Analysis of a Self-Starting Three-Dimensional Scramjet Intake
Boundary Layer Ingestion Propulsion Benefit for Transport Aircraft
Characterizing Propellants for Variable-Thrust/Specific Impulse Colloid Thrusters
Uncertainty Quantification for Fat-Tailed Probability Distributions in Aircraft Engine Simulations
Uncertainty Quantification for Fat-Tailed Probability Distributions in Aircraft Engine Simulations
Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield
Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield
Design of a Premixed Fuel–Oxidizer System to Arrest Flashback in a Rotating Detonation Engine
Design of a Premixed Fuel–Oxidizer System to Arrest Flashback in a Rotating Detonation Engine
Flow Rate Measurement Method for Gaseous Fuel Injection for Pulse Detonation Engines
Numerical Investigation of Shrouded Ejector-Enhanced Pulse Combustor Performance at High Pressure
Numerical Investigation of Shrouded Ejector-Enhanced Pulse Combustor Performance at High Pressure
Measurement of Impulsive Thrust from a Closed Radio-Frequency Cavity in Vacuum
Measurement of Impulsive Thrust from a Closed Radio-Frequency Cavity in Vacuum
Simulations of Ion Thruster Plumes in Ground Facilities Using Adaptive Mesh Refinement
Simulations of Ion Thruster Plumes in Ground Facilities Using Adaptive Mesh Refinement
Diffusion-Flame Ignition by Shock-Wave Impingement on a Hydrogen–Air Supersonic Mixing Layer
Optimization of Blockerless Engine Thrust Reverser
Optimization of Blockerless Engine Thrust Reverser
Combustion Dynamics in Postchamber of Hybrid Rocket Using
Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor
Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor
Dynamic Characteristics of Open-Type Swirl Injector with Varying Geometry
Inward-Turning Streamline-Traced Inlet Design Method Low-Boom Low-Drag Applications
Inward-Turning Streamline-Traced Inlet Design Method Low-Boom Low-Drag Applications