Call Number (LC) Title Results
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
Y 3.N 21/5:8/737 Conversion of energy in cross-sectional divergences under different conditions of inflow / 1
Y 3.N 21/5:8/738 Investigation of a Rateau supercharger for a 700-horsepower airplane engine / 1
Y 3.N 21/5:8/739 Experiments with planing surfaces / 1
Y 3.N 21/5:8/740 The development of floats and equipment for research in promoting it / 1
Y 3.N 21/5:8/741 The calculation of lateral stability with free controls / 1
Y 3.N 21/5:8/742 Supplemental data and calculations of the lateral stability of airplanes / 1
Y 3.N 21/5:8/743 Fatigue strength of airplane an engine materials / 1
Y 3.N 21/5:8/744 Torsional stresses in box beams with cross sections partially restrained against warping / 1
Y 3.N 21/5:8/745 High-speed aircraft / 1
Y 3.N 21/5:8/746 The high-speed Heinkel HE 70 mail airplane / 1
Y 3.N 21/5:8/747 Analysis of spinning in a monoplane wing by the induction method as compared with the strip method / 1
Y 3.N 21/5:8/748 Impact buckling of thin bars in the elastic range hinged at both ends / 1
Y 3.N 21/5:8/749 Impact buckling of thin bars in the elastic range for any end condition / 1
Y 3.N 21/5:8/750 Influence of cut-outs in elevator on the static longitudinal stability and on the static elevator effect / 1
Y 3.N 21/5:8/751 Investigation of boundary layers on an airplane wing in free flight / 1
Y 3.N 21/5:8/752 Additional test data on static longitudinal stability / 1
Y 3.N 21/5:8/753 Stipa monoplane with venturi fuselage / 1