| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:8/1190 | Tests of cascades of airfoils for retarded flow / | 1 |
| Y 3.N 21/5:8/1191 | Venturi tube with varying mass flow / | 1 |
| Y 3.N 21/5:8/1192 | Rotating disks in the region of permanent deformation / | 1 |
| Y 3.N 21/5:8/1193 | Measurements on compressor-blade lattices / | 1 |
| Y 3.N 21/5:8/1194 |
Force- and pressure-distribution measurements on eight fuselages / Force- and pressure-distribution measurements on eight fuselages, October 1948. |
2 |
| Y 3.N 21/5:8/1195 | On the sound field of a rotating propeller / | 1 |
| Y 3.N 21/5:8/1196 | Nonstationary gas flow in thin pipes of variable cross section / | 1 |
| Y 3.N 21/5:8/1197 | Investigations on the stability, oscillation, and stress conditions of airplanes with tab control. : First partial report - Derivation of the equations of motion and their general solutions / | 1 |
| Y 3.N 21/5:8/1198 | Investigations on the stability, oscillation, and stress conditions of airplanes with tab control. : Second partial report - Application of the solutions obtained in the First Partial Report to tab-controlled airplanes / | 1 |
| Y 3.N 21/5:8/1200 | Measurement of oil-film pressures in journal bearings under constant and variable loads / | 1 |
| Y 3.N 21/5:8/1201 | Rotation in free fall of rectangular wings of elongated shape / | 1 |
| Y 3.N 21/5:8/1203 | The compressible flow past various plane profiles near sonic velocity / | 1 |
| Y 3.N 21/5:8/1204 | Some new problems on shells and thin structures / | 1 |
| Y 3.N 21/5:8/1205 | Exact calculation of laminar boundary layer in longitudinal flow over a flat plate with homogeneous suction / | 1 |
| Y 3.N 21/5:8/1206 | Systematic investigations of the effects of plan form and gap between the fixed surface and control surface on simple flapped wings / | 1 |
| Y 3.N 21/5:8/1207 | The theory of plasticity in the case of simple loading accompanied by strain-hardening / | 1 |
| Y 3.N 21/5:8/1208 | Calculation of counterrotating propellers / | 1 |
| Y 3.N 21/5:8/1209 | Experimental study of flow past turbine blades / | 1 |
| Y 3.N 21/5:8/1210 | Development of spoiler controls for remote control of flying missiles / | 1 |
| Y 3.N 21/5:8/1211 | The characteristics method applied to stationary two-dimensional and rotationally symmetrical gas flows / | 1 |
