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- Tests of a small-scale NACA submerged inlet at transonic Mach numbers
- Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8
- Preliminary attempts at isothermal compression of a supersonic air stream
- Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics
- Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8
- Effects on adjacent surfaces from the firing of rocket jets