PROPULSION REQUIREMENTS FOR FUTURE GENERATION SPACE HABITATS
COMPUTATIONAL INLET SWIRL DISTORTION INVESTIGATION OF A HIGH-SPEED COMPRESSOR
NUMERICAL INVESTIGATION OF A SWIRL INDUCED FLAMELESS COMBUSTOR FOR GAS TURBINE APPLICATIONS
PROPULSION SYSTEM DESIGN FOR MARS ASCENT VEHICLES BY USING THE IN-SITU CO2
AIRCRAFT ENGINE PERFORMANCE MODEL IDENTIFICATION USING ARTIFICIAL NEURAL NETWORKS
NUMERICAL AND EXPERIMENTAL ANALYSIS OF A SINGLE STAGE DRONE JET ENGINE
DESCRIPTION AND APPLICATION OF A SOFTWARE TOOL FOR SIMULATION OF TOMOGRAPHIC PIV DATA
DESIGN CONSIDERATIONS FOR EXTRA HIGH-PRESSURE RATIO (70) CIVIL AERO ENGINE LOW-EMISSION COMBUSTOR
A SIMPLIFIED MODEL FOR THE THRUST PERFORMANCE OF POROUS HEAT EXCHANGER (PHX) LASER ROCKET PROPULSION
DEFLAGRATION TO DETONATION TRANSITION IN CHEMICAL ROCKETS WITH SUDDEN EXPANSION/DIVERGENCE REGION
POSSIBLE EFFECTS OF TURBINE/FUEL CELL INTEGRATION ON COMBUSTOR OPERATION
DESIGN, ANALYSIS, AND TESTING OF A LOW-COST, ADDITIVELY-MANUFACTURED, SINGLE-USE COMRESSOR
ANALYSIS OF A COMPACT COMBUSTOR FOR USE IN A JETCAT P90 RXI