Call Number (LC) Title Results
Y 3.N 21/5:8/717 Development of the rules governing the strength of airplanes. : Part 2. Loading conditions in Germany (continued), England, and the United States / 1
Y 3.N 21/5:8/718 Development of the rules governing the strength of airplanes. : Part 3. Loading conditions in France, Italy, Holland, and Russia - Aims at standardization / 1
Y 3.N 21/5:8/719 Dimensions of twin seaplane floats / 1
Y 3.N 21/5:8/720 Recent results of turbulence research / 1
Y 3.N 21/5:8/721 Results of extended tests of the Focke-Wulf F 19a "Ente", a tail-first airplane / 1
Y 3.N 21/5:8/722 Guide vanes for deflecting fluid currents with small loss of energy / 1
Y 3.N 21/5:8/723 An airfoil spanning an open jet / 1
Y 3.N 21/5:8/724 The 1933 contest for the Deutsch de la Meurthe trophy / 1
Y 3.N 21/5:8/725 Development of air-cooled engines with blower cooling / 1
Y 3.N 21/5:8/726 Attaining a steady air stream in wind tunnels / 1
Y 3.N 21/5:8/727 The theory of the Strandgren cyclogiro / 1
Y 3.N 21/5:8/728 Aerodynamic forces and moments of a seaplane on the water / 1
Y 3.N 21/5:8/729 The flight of an autogiro at high speed / 1
Y 3.N 21/5:8/730 Practical experiences with lightning discharges to airplanes / 1
Y 3.N 21/5:8/731 Trend of airplane flight characteristics / 1
Y 3.N 21/5:8/732 Evaluation of scavenging in two-stroke-cycle engines / 1
Y 3.N 21/5:8/733 Aerodynamic principles of the direct lifting propeller / 1
Y 3.N 21/5:8/734 The small wind tunnel of the DVL / 1
Y 3.N 21/5:8/735 The high-speed tank of the Hamburg shipbuilding company / 1
Y 3.N 21/5:8/736 Effect of fuselage and engine nacelles on some aerodynamic properties of an airplane wing / 1