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- Experimental investigation of pressure fluctuations in 3.6 inch ram jet at Mach number 1.92
- Effect of ram-jet pressure pulsations on supersonic-diffuser performance
- Some observations of flow at the throat of a two-dimensional diffuser at a Mach number of 3.85
- Experimental investigation of a two-dimensional split-wing ram-jet inlet at Mach number of 3.85
- Performance characteristics of several types of axially symmetric nose inlets at Mach number 3.85
- Preliminary investigation of an asymmetric swept nose inlet of circular projection at Mach number 3.85
- Characteristics of flow about axially symmetric isentropic spikes for nose inlets at Mach number 3.85
- Preliminary investigation of an asymmetric swept nose inlet of circular projection at Mach number 3.85
- Force, moment, and pressure characteristics of several annular nose inlets at Mach number 3.85
- Interferometric observation of flow about an isentropic (reverse Prandtl-Meyer streamline) compression wedge at Mach 3.0
- Performance characteristics of axisymmetric two-cone and isentropic nose inlets at Mach number 1.90
- A variable-geometry axisymmetric supersonic inlet with telescoping centerbody
- A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05
- Some aspects of supersonic inlet stability
- Design Criteria for Axisymmetric and Two-Dimensional Supersonic Inlets and Exits
- Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air
- Investigation of translating-double-cone axisymmetric inlets with cowl projected areas 40 and 20 percent of maximum at Mach numbers from 3.0 to 2.0
- Effects of Internal-Area Distribution, Spike Translation, and Throat Boundary-Layer Control on Performance of a Double-Cone Axisymmetric Inlet at Mach Numbers From 3.0 to 2.0
- Survey of supersonic inlets for high Mach number applications
- Survey of Supersonic Inlets for High Mach Number Applications
- High Mach Number, Low-Cowl-Drag, External-Compression Inlet With Subsonic Dump Diffuser
- High Mach Number, Low-Cowl-Drag, External-Compression Inlet With Subsonic Dump Diffuser