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
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