Call Number (LC) Title Results
Y3.N21_5..8_866 Calculation of load distribution in stiffened cylindrical shells. 1
Y3.N21_5..8_867 Theoretical study of various airplane motions after initial disturbance. 1
Y3.N21_5..8_868 The Dornier wind tunnel. 1
Y3.N21_5..8_869 Conversion of energy in a radiator. 1
Y3.N21_5..8_870 Behavior of plate strip under shear and compressive stresses beyond buckling limit. 1
Y3.N21_5..8_871 Performance of rotating-wing aircraft. 1
Y3.N21_5..8_872 Present status of airship construction, especially of airship-framing construction. 1
Y3.N21_5..8_873 Experimental study of ignition by hot spot in internal combustion engines. 1
Y3.N21_5..8_874 Effect of propeller slipstream on wing and tail. 1
Y3.N21_5..8_875 Heat-stressed structural components in combustion-engine design. 1
Y3.N21_5..8_876 Investigations on the downwash behind tapered wing with fuselage and propeller. 1
Y3.N21_5..8_877 Wind℗--tunnel investigations on flexural-torsional wing flutter. 1
Y3.N21_5..8_878 Twisting of thin-walled, stiffened circular cylinders. 1
Y3.N21_5..8_879 Static longitudinal stability and longitudinal control of autogiro rotors. 1
Y3.N21_5..8_880 Effective width of curved sheet after buckling. 1
Y3.N21_5..8_881 Application and testing of transparent plastics used in airplane construction. 1
Y3.N21_5..8_882 Modern manufacturing equipment of Ernst Heinkel Airplane Works. 1
Y3.N21_5..8_883 Distribution of temperatures over an airplane wing with reference to phenomena of ice formation. 1
Y3.N21_5..8_884 Calculation of induced efficiency of heavily loaded propellers having infinite number of blades; Induced efficiency of optimum propellers having finite number of blades; Prospects of propeller drive for high flying speeds. 1
Y3.N21_5..8_885 Meteorological-physical limitations of icing in the atmosphere. 1