Call Number (LC) Title Results
Y 3.N 21/5:6/64 N.A.C.A. recording air speed meter / 1
Y 3.N 21/5:6/65 Langley Field wind tunnel apparatus / 1
Y 3.N 21/5:6/66 Gőttingen wind tunnel for testing aircraft models / 1
Y 3.N 21/5:6/67 Ground influence on aerofoils / 1
Y 3.N 21/5:6/68 Vortices and the related principles of hydrodynamics / 1
Y 3.N 21/5:6/69 An investigation on the effect of raked wing tips / 1
Y 3.N 21/5:6/70 The effect of staggering a biplane / 1
Y 3.N 21/5:6/71 Experiments with slotted wings. 1
Y 3.N 21/5:6/72 Aneroid investigations in Germany. 1
Y 3.N 21/5:6/73 The choice of wing sections for airplanes / 1
Y 3.N 21/5:6/74 Mutual influence of wings and propellers / 1
Y 3.N 21/5:6/75 Effects of varying the relative vertical position of wing and fuselage / 1
Y 3.N 21/5:6/76 A mechanical device for illustrating airplane stability / 1
Y 3.N 21/5:6/77 A preliminary investigation of a new method for testing aerofoils in free flight / 1
Y 3.N 21/5:6/78 Impact tests for woods / 1
Y 3.N 21/5:6/79 Effect of aerofoil aspect ratio on the slope of the lift curve / 1
Y 3.N 21/5:6/80 The dead weight of the airship and the number of passengers that can be carried / 1
Y 3.N 21/5:6/81 Langley Field wind tunnel apparatus. 1
Y 3.N 21/5:6/82 Notes on the construction and testing of model airplanes / 1
Y 3.N 21/5:6/83 The theory of the screw propeller / 1