Numerical investigation of the split sliding guide vane for a variable nozzle turbine
Busemann diffuser for supersonic ramjet on detonation combustion of kerosene vapor
Multi-objective aerodynamic optimization of expansion–deflection nozzle based on B-spline curves
Effects of Nozzle Orifice Diameter and Hole Number on Diesel Combustion and Engine Performance
An empirical model for partially admitted turbine efficiency
Proposed Flight Research of a Dual-Bell Rocket Nozzle Using the NASA F-15 Airplane
Experimental research of the small gas turbine with variable area nozzle
Computational and Experimental Study of Nozzle Performance for Rotating Detonation Rocket Engines
Proposed Flight Research of a Dual-Bell Rocket Nozzle Using the NASA F-15 Airplane
Effect of ceramic nozzle on performance of pulsed plasma thruster
Experimental Demonstration of the Vacuum Specific Impulse of a Hybrid Rocket Engine
On a Variable Nozzle for Limited Hot Gas Flows
Decomposing Solid Micropropulsion Nozzle Performance Issues
Nozzle performance evaluation program Final report
Benefits of Spin Polarization for Inertial and Magneto-Inertial Fusion Propulsion