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- Air-flow surveys in the vicinity of representative NACA 1-series cowlings
- Tests of a small-scale NACA submerged inlet at transonic Mach numbers
- A survey of methods for turbojet thrust measurement applicable to flight installation
- Preliminary attempts at isothermal compression of a supersonic air stream
- Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles
- Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds
- Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds
- A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05
- Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas
- Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air
- An inlet design concept to reduce flow distortion at angle of attack
- Comparison of experimentally and analytically determined windmilling characteristics of a compressor with low over-all pressure ratio
- Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds