TECHNICAL NOTES - Direct-Drive System Demonstration for a Low-Power Hall Thruster
Wall Temperature Effects on Heat Transfer Coefficient for High-Pressure Turbines
Damping Coefficient Prediction of Solid Rocket Motor Nozzle Using Computational Fluid Dynamics
Forced Response of Mistuned Bladed Disks: Quantitative Validation of the Asymptotic Description
Acoustic Simulation of Hot Jets Issuing from a Rectangular Hypersonic Nozzle
Design of an Asymmetric Scramjet Nozzle with Circular to Rectangular Shape Transition
Oxidation of Ethylene — Air Mixtures at Elevated Pressures, Part 2: Chemical Kinetics
Numerical Simulation of Dome Filling in an Experimental Rocket Engine Mockup