Healed Without Scars

Visual Study of Swirling and Nonswirling Two-phase Two-component Flow at 1 and 0 Gravity

Visual Study of Swirling and Nonswirling Two-phase Two-component Flow at 1 and 0 Gravity

Analysis of Topping and Bleed Turbopump Units for Hydrogen-propelled Nuclear Rockets

Turbine Aerodynamic and Cooling Requirements for a Turbojet Powered Mach 3 Transport Using Methane Fuel

A Method for Determining Turbine Design Characteristics for Rocket Turbodrive Applications

Cold-air Performance Evaluation of Scale Model Oxidizer Pump-drive Turbine for the M-1 Hydrogen-oxygen Rocket Engine: Overall two-stage performance. II