Effect of Chord Size on Weight and Cooling Characteristics of Air-cooled Turbine Blades
Effect of Diameter of Closed-end Coolant Passages on Natural-convection Water Cooling of Gas-turbine Blades
Some Factors Influencing Heat Transfer to Liquid-propellant Rocket-thrust-chamber Coolant Channels
An Experimental Investigation of Sting-support Effects on Drag and a Comparison with Jet Effects at Transonic Speeds
Effect of Blade-tip Crossover Passages on Natural-convection Water-cooling of Gas-turbine Blades
Analysis of Effects of Rocket-engine Design Parameters on Regenerative-cooling Capabilities of Several Propellants
Analysis of Effects of Rocket-engine Design Parameters on Regenerative-cooling Capabilities of Several Propellants
Description and Expected Performance of Flight-model, 12-gigahertz, Output Stage Tube for the Communications Technology Satellite
A Balanced-pressure Sliding Seal for Transfer of Pressurized Air Between Stationary and Rotating Parts
Some Factors Influencing Heat Transfer to Liquid-propellant Rocket-thrust-chamber Coolant Channels
Secondary Electron Emission Characteristics of Ion-textured Copper and High-purity Isotropic Graphite Surfaces
Thermal Anomalies of the Transmitter Experiment Package on the Communications Technology Satellite
Textured Carbon on Copper
Plasma Tests of Sprayed Coatings for Rocket Thrust Chambers
Comparison of Pressure-loss Characteristics of Several Tail-cone Air-induction Systems for Air-cooled Gas-turbine Rotors