Call Number (LC) | Title | Results |
---|---|---|
Y 3.N 21/5:8/867 |
Theoretical study of various airplane motions after initial disturbance / Theoretical study of various airplane motions after initial disturbance. |
2 |
Y 3.N 21/5:8/868 |
The Dornier wind tunnel / The Dornier wind tunnel. |
2 |
Y 3.N 21/5:8/869 |
The conversion of energy in a radiator / Conversion of energy in a radiator. |
2 |
Y 3.N 21/5:8/870 |
Behavior of a plate strip under shear and compressive stresses beyond the buckling limit / Behavior of plate strip under shear and compressive stresses beyond buckling limit. |
2 |
Y 3.N 21/5:8/871 |
Performance of rotating-wing aircraft / Performance of rotating-wing aircraft. |
2 |
Y 3.N 21/5:8/872 |
The present status of airship construction, especially of airship-framing construction / Present status of airship construction, especially of airship-framing construction. |
2 |
Y 3.N 21/5:8/873 |
Experimental study of ignition by hot spot in internal combustion engines / Experimental study of ignition by hot spot in internal combustion engines. |
2 |
Y 3.N 21/5:8/874 |
Effect of propeller slipstream on wing and tail / Effect of propeller slipstream on wing and tail. |
2 |
Y 3.N 21/5:8/875 |
Heat-stressed structural components in combustion-engine design / Heat-stressed structural components in combustion-engine design. |
2 |
Y 3.N 21/5:8/876 |
Investigations on the downwash behind a tapered wing with fuselage and propeller / Investigations on the downwash behind tapered wing with fuselage and propeller. |
2 |
Y 3.N 21/5:8/877 |
Wind-tunnel investigations on flexural-torsional wing flutter / Windâ„—--tunnel investigations on flexural-torsional wing flutter. |
2 |
Y 3.N 21/5:8/878 |
The twisting of thin-walled, stiffened circular cylinders / Twisting of thin-walled, stiffened circular cylinders. |
2 |
Y 3.N 21/5:8/879 |
Static longitudinal stability and longitudinal control of autogiro rotors / Static longitudinal stability and longitudinal control of autogiro rotors. |
2 |
Y 3.N 21/5:8/880 |
The effective width of curved sheet after buckling / Effective width of curved sheet after buckling. |
2 |
Y 3.N 21/5:8/881 |
Application and testing of transparent plastics used in airplane construction / Application and testing of transparent plastics used in airplane construction. |
2 |
Y 3.N 21/5:8/882 |
Modern manufacturing equipment of the Ernest Heinkel airplane works / Modern manufacturing equipment of Ernst Heinkel Airplane Works. |
2 |
Y 3.N 21/5:8/883 |
Distribution of temperatures over an airplane wing with reference to the phenomena of ice formation / Distribution of temperatures over an airplane wing with reference to phenomena of ice formation. |
2 |
Y 3.N 21/5:8/884 |
Calculation of the induced efficiency of heavily loaded propellers having infinite number of blades / 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. |
2 |
Y 3.N 21/5:8/885 |
Meteorological-physical limitations of icing in the atmosphere / Meteorological-physical limitations of icing in the atmosphere. |
2 |
Y 3.N 21/5:8/886 |
Theory of two-dimensional potential flow about arbitrary wing sections / Theory of two-dimensional potential flow about arbitrary wing sections. |
2 |