W. A. P. Fisher

• A parameter to represent the mechanical properties of aluminium alloys after soaking at elevated temperatures
• Aircraft manoeuvre loads
• Experimental correlation between the endurance of a wing spar joint and the ratio between 0.1 per cent proof and ultimate tensile strengths of the material
• Fatigue tests on notched extruded aluminium alloy (DTD364B) having a theoretical stress concentration factor of 3.65
• Programme fatigue tests on notched bars to a gust load spectrum
• Some fatigue tests on notched specimens with programme loading for a "ground-attack" aircraft