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- Analysis of heat addition in a convergent-divergent nozzle
- Investigation at supersonic speeds of an inlet employing conical flow separation from a probe ahead of a blunt body
- Thrust and Pumping Characteristics of a Series of Ejector-type Exhaust Nozzles at Subsonic and Supersonic Flight Speeds
- Thrust and pumping characteristics of a series of ejector-type exhaust nozzles at subsonic and supersonic flight speeds
- Investigation of thrust and drag characteristics of a plug-type exhaust nozzle
- Thrust and drag characteristics of a convergent-divergent nozzle with various exhaust jet temperatures
- Performance of a 16-inch ram-jet engine with a can-type combustor at Mach numbers of 1.50 to 2.16
- Application of oblique-shock sensing system to ram-jet-engine flight Mach number control
- Matching of auxiliary inlets to secondary-air requirements of aircraft ejector exhaust nozzles
- Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles
- Exhaust Nozzles for Supersonic Flight with Turbojet Engines
- Performance comparison at Mach numbers 1.8 and 2.0 of full-scale and quarter-scale translating-spike inlets
- Investigation of a supersonic-inlet - turbojet-engine combination at Mach 2.0 and angles of attack up to 6 degrees
- Use of main-inlet bypass to supply ejector exhaust nozzle at supersonic speeds
- Use of constant diffuser Mach number as a control parameter for variable-geometry inlets at Mach numbers of 1.8 to 2.0
- Performance Comparison at Mach Numbers 1.8 and 2.0 of Full Scale and Quarter Scale Translating-Spike Inlets
- Use of Constant Diffuser Mach Number as a Control Parameter for Variable-Geometry Inlets at Mach Numbers of 1.8 to 2.0
- A performance analysis of methods for handling excess inlet flow at supersonic speeds