Call Number (LC) Title Results
Y 3.N 21/5:8/1313 On the recording of turbulent longitudinal and transverse fluctuations / 1
Y 3.N 21/5:8/1314 On the turbulent friction layer for rising pressure / 1
Y 3.N 21/5:8/1315 Displacement effect of the laminar boundary layer and the pressure drag / 1
Y 3.N 21/5:8/1316 Resistance of a plate in parallel flow at low Reynolds numbers / 1
Y 3.N 21/5:8/1317 A simple numerical method for the calculation of the laminar boundary layer / 1
Y 3.N 21/5:8/1318 Friction and wear / 1
Y 3.N 21/5:8/1319 Torsion and bending of prismatic rods of hollow rectangular section / 1
Y 3.N 21/5:8/1320 Investigations on wings with and without sweepback at high subsonic speeds / 1
Y 3.N 21/5:8/1321 Relations between the modulus of elasticity of binary alloys and their structure / 1
Y 3.N 21/5:8/1322 Theory of thin-walled rods / 1
Y 3.N 21/5:8/1323 Influence of static longitudinal stability on the behavior of airplanes in gusts / 1
Y 3.N 21/5:8/1324 Steady vibrations of wing of circular plan form : and Theory of wing of circular plan form / 1
Y 3.N 21/5:8/1325 Concerning the flow about ring-shaped cowlings of finite thickness. : Part 1 / 1
Y 3.N 21/5:8/1326 Concerning the flow about ring-shaped cowlings. : Part 2 - Annular bodies of infinite length with circulation for smooth entrance / 1
Y 3.N 21/5:8/1327 Concerning the flow about ring-shaped cowlings. : Part 6 - Further measurements on inlet devices / 1
Y 3.N 21/5:8/1328 Concerning the flow about ring-shaped cowlings. : Part 8 - Further measurements on annular profiles / 1
Y 3.N 21/5:8/1329 Concerning the flow about ring-shaped cowlings. : Part 9 - The influence of oblique oncoming flow on the incremental velocities and air forces at the front part of circular cowls / 1
Y 3.N 21/5:8/1330 Theory of dynamic creep / 1
Y 3.N 21/5:8/1331 Investigations of the boundary-layer control on a full scale swept wing with air bled off from the turbojet / 1
Y 3.N 21/5:8/1332 Extension to the cases of two dimensional and spherically symmetric flows of two particular solutions to the equations of motion governing unsteady flow in a gas / 1