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- A Preliminary Investigation at Mach Number 1.91 of an Inlet Configuration Designed for Insensitivity to Positive Angle-of-Attack Operation
- A Preliminary Investigation at Mach Number 1.91 of a Diffuser Employing a Pivoted Cone to Improve Operation at Angle of Attack
- Effects of a J34 turbojet engine on supersonic diffuser performance
- Effects of Rocket-Armament Exhaust Gas on the Performance of a Supersonic-Inlet J34-Turbojet-Engine Installation at Mach 2.0
- Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet
- Performance of Twin-Duct Variable-Geometry Side Inlets at Mach Numbers of 1.5 to 2.0
- Performance of Twin-Duct Variable-Geometry Side Inlets at Mach Numbers of 1.5 to 2.0
- Off-Design Performance of Divergent Ejectors
- Investigation of Control Signals for Variable Ramps of Twin-Duct Side Inlets
- Off-Design Performance of Divergent Ejectors
- Investigation of Control Signals for Variable Ramps of Twin-Duct Side Inlets