Burning Rate Optimization Under Uncertainty Using Response Surfaces and Monte Carlo Simulation
FULL-LENGTH PAPERS - Influence of Initial Propellant Temperature on Solid Rocket Internal Ballistics
Ignition Transients in a Scramjet Engine with Air Throttling Part 1: Nonreacting Flow
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
Unsteady Vane Boundary Layer Response to Rotor-Rotor Interactions in a Multistage Compressor
Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster
TECHNICAL NOTES - Direct-Drive System Demonstration for a Low-Power Hall Thruster