Radiation Shielding for Manned Space Flight
Reynolds Number Effect on Axial-flow Compressor Performance
Radiation Shielding for Manned Space Flight
Preliminary Results of an Altitude-wind-tunnel Investigation of an Axial-flow Gas Turbine-propeller Engine
Analysis of Thermal-protection Systems for Space-vehicle Cryogenic-propellant Tanks
Some Effects of Transients in Inlet Pressure and Temperature on Turbojet Engines
Generalization of Turbojet and Turbine-propeller Engine Performance in Windmilling Condition
EVALUATION OF AN AUTOMATIC INLET-PRESSURE CONTROL VALVE FOR STUDY OF TRANSIENT ENGINE PERFORMANCE CHARACTERISTICS.
A Study of Temperature Transients at the Inlet of a Turbojet Engine
Preliminary Results of an Altitude-wind-tunnel Investigation of an Axial-flow Gas Turbine-propeller Engine
Investigation of Performance of Turbojet Engine with Constant- and Variable-area Exhaust Nozzles
Full-scale Investigation of Cooling Shroud and Ejector Nozzle for a Turbojet Engine - Afterburner Installation
Acceleration Characteristics of a Turbojet Engine with Variable-position Inlet Guide Vanes
Effect of Compressor-outlet Bleedoff on Turbojet-engine Performance
Experimental Investigation of Typical Constant- and Variable-area Exhaust Nozzles and Effects on Axial-flow Turbojet-engine Performance
Effect of Uneven Air-flow Distribution to the Twin Inlets of an Axial-flow Turbojet Engine
Steady-state and Surge Characteristics of a Compressor Equipped with Variable Inlet Guide Vanes Operating in a Turbojet Engine
Effect of Inlet-duct Length in Uniform-flow Field on Turbojet-engine Operation