A. B. Haines

• Scale effects at high subsonic and transonic speeds, and methods for fixing boundary-layer transition in model experiments
• Scale effects on aircraft and weapon aerodynamics
• Some notes on the flow patterns observed over various swept-back wings at low Mach numbers (in the R.A.E. 10-ft x 7-ft high speed tunnel)
• Tests in the Royal Aircraft Establishment 10-ft x 7-ft high-speed tunnel on 50-deg swept-back wings. Part I. Three of 7.5 per cent thickness. Part II. One of 7.5 per cent thickness with stall fences and leading-edge chord extension
• The centre line Mach number distributions and auxiliary suction requirements for the A.R.A. 9ft. x 8ft. transonic wind tunnel