Call Number (LC) Title Results
Y 3.N 21/5:8/555 The boundary layer as a means of controlling the flow of liquids and gases / 1
Y 3.N 21/5:8/556 The electrodynamometric balance of the small wind tunnel of the French Service of Aeronautical Research / 1
Y 3.N 21/5:8/557 Measurement of profile drag on an airplane in flight by the momentum method. : Part 1 / 1
Y 3.N 21/5:8/558 Measurement of profile drag on an airplane in flight by the momentum method. : Part 2 / 1
Y 3.N 21/5:8/559 Ratier metal propeller with pitch variable in flight / 1
Y 3.N 21/5:8/560 The 1929 Rhon soaring-flight contest / 1
Y 3.N 21/5:8/561 Improving the performance of multi-engined airplanes by means of idling propellers. : The "free-wheel" propeller / 1
Y 3.N 21/5:8/562 Experimental investigation of aircraft propellers exposed to oblique air currents / 1
Y 3.N 21/5:8/563 Balanced and servo control surfaces. 1
Y 3.N 21/5:8/564 Recent tests of tailless airplanes / 1
Y 3.N 21/5:8/565 Development of the Junkers-Diesel aircraft engine / 1
Y 3.N 21/5:8/566 Experimental research on the friction of pivots / 1
Y 3.N 21/5:8/567 The Magnus Effect in theory and in reality / 1
Y 3.N 21/5:8/568 Contribution to the theory of propeller vibrations / 1
Y 3.N 21/5:8/569 A possible method for preventing the autorotation of airplane wings / 1
Y 3.N 21/5:8/570 "Gloster" metal construction. 1
Y 3.N 21/5:8/571 Propulsion by reaction / 1
Y 3.N 21/5:8/572 Impact tests on rubber compression springs for airplane landing gears / 1
Y 3.N 21/5:8/573 Air forces and air-force moments at large angles of attack and how they are affected by the shape of the wing / 1
Y 3.N 21/5:8/574 Calculation of pressure distribution on airship hulls / 1