Grace Huntley
Effect of Circumferential Total-pressure Gradients Typical of Single-inlet Duct Installations on Performance of an Axial-flow Turbojet Engine
Effect of Variable-position Inlet Guide Vanes and Interstage Bleed on Compressor Performance of a High-pressure-ratio Turbojet Engine
Effect of Inlet-air Baffles on Rotating-stall and Stress Characteristics of an Axial-flow Compressor in a Turbojet Engine
Component and Over-all Performance Evaluation of an Axial-flow Turbojet Engine Over a Range of Engine-inlet Reynolds Numbers
Combined Compressor Coolant Injection and Afterburner for Turbojet Thrust Augmentation
Comparison of Locked-rotor and Windmilling Drag Characteristics of an Axial-flow-compressor Type-turbojet Engine
Results of Christmas Examinations, 1939 : Second Year Degree, OAC Review, V.51, No.4, January 1939, Pages 268-269
Altitude Performance Investigation of Two Flame-holder and Fuel-system Configurations in Short Afterburner
Results of Final Examinations, 1939 : Second Year Degree, OAC Review, V.51, No.7, May 1939, Pages 454-456
Results of Final Examinations, 1939
Altitude Performance Investigation of a High-temperature Afterburner
Ideal Temperature Rise Due to Constant-pressure Combustion of a JP-4 Fuel
C.O.T.C. Communique
Results of Christmas Examinations, 1939
Pumping and Thrust Characteristics of Several Divergent Cooling-air Ejectors and Comparison of Performance with Conical and Cylindrical Ejectors
Results of Christmas Examinations, 1937
The Proceedings of the 1994 Petroleum Hydrocarbons and Organic Chemicals in Ground Water : Prevention, Detection, and Remediation - Conference; Houston, TX, November 2 - 4 1994 (National Ground Water Association
Real Life
Conscious, Choices, Unconscious Forces