Call Number (LC) | Title | Results |
---|---|---|
Y 3.N 21/5:8/801 |
Correction of downwash in wind tunnels of circular and elliptic sections / Correction of downwash in wind tunnels of circular and elliptic sections. |
2 |
Y 3.N 21/5:8/802 |
Automatic stabilization / Automatic stabilization. |
2 |
Y 3.N 21/5:8/803 |
Details of the construction and production of fuel pumps and fuel nozzles for the airplane diesel engines / Details of the construction and production of fuel pumps and fuel nozzles for the airplane Diesel engine. |
2 |
Y 3.N 21/5:8/804 |
The stress criterion of a tension member with graded flexural stiffness (contribution to the problem of "clamping effect" outside of the elastic range) The stress criterion of a tension member with graded flexural stiffness. : (contribution to the problem of "clamping effect" outside of the elastic range) / |
2 |
Y 3.N 21/5:8/805 |
General considerations on the flow of compressible fluids / General considerations on the flow of compressible fluids. |
2 |
Y 3.N 21/5:8/806 |
The question of spontaneous wing oscillations. : (Determination of critical velocity through flight-oscillation tests) / The question of spontaneous wing oscillations (determination of critical velocity through flight-oscillation tests) |
2 |
Y 3.N 21/5:8/807 |
Torsion and buckling of open sections / Torsion and buckling of open sections. |
2 |
Y 3.N 21/5:8/808 | High-speed wind tunnels / | 1 |
Y 3.N 21/5:8/809 |
Tests for the determination of the stress condition in tension fields / Tests for the determination of the stress condition in tension fields. |
2 |
Y 3.N 21/5:8/810 |
Impact of a vee-type seaplane on water with reference to elasticity / Impact of a Vee℗--type seaplane on water with reference to elasticity. |
2 |
Y 3.N 21/5:8/811 |
The impact on floats or hulls during landing as affected by bottom width / The impact on floats or hulls during landing as affected by bottom width. |
2 |
Y 3.N 21/5:8/812 |
The horsepower of aircraft engines and their maximum frontal area / The horsepower of aircraft engines and their maximum frontal area. |
2 |
Y 3.N 21/5:8/813 |
The cetene scale and the induction period preceding the spontaneous ignition of diesel fuels in bombs / The cetene scale and the induction period preceding the spontaneous ignition of diesel fuels in bombs. |
2 |
Y 3.N 21/5:8/814 |
Experimental studies of the effective width of buckled sheets / Experimental studies of the effective width of buckled sheets. |
2 |
Y 3.N 21/5:8/815 |
Automatic stabilization / Automatic stabilization. |
2 |
Y 3.N 21/5:8/816 |
The gyroplane - its principles and its possibilities / The gyroplane--its principles and its possibilities. |
2 |
Y 3.N 21/5:8/817 | The stress distribution in shell bodies and wings as an equiilibrium problem / | 1 |
Y 3.N 21/5:8/818 |
Valve-spring surge / Valve-spring surge. |
2 |
Y 3.N 21/5:8/819 |
Experimental apparatus for the study of propellers / Experimental apparatus for the study of propellers. |
2 |
Y 3.N 21/5:8/820 |
Some experiments on the slipstream effect / Some experiments on the slipstream effect. |
2 |