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- Flight tests of a balanced split flap with particular reference to rapid operation
- Flight tests of an airplane showing dependence of the maximum lift coefficient on the test conditions
- Improvement of aileron effectiveness by the prevention of air leakage through the hinge gap as determined in flight
- A flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design
- Design charts relating to the stalling of tapered wings
- Preliminary investigation of the flying qualities of airplanes