Call Number (LC) Title Results
Y 3.N 21/5:8/1174 Analytical treatment of normal condensation shock / 1
Y 3.N 21/5:8/1175 Fundamental aerodynamic investigations for development of arrow-stabilized projectiles / 1
Y 3.N 21/5:8/1176 Test report on three- and six-component measurements on a series of tapered wings of small aspect ratio : (Partial Report: Triangular wings) / 1
Y 3.N 21/5:8/1177 Wind-tunnel investigations on a changed Mustang profile with nose flap. : Force and pressure-distribution measurements / 1
Y 3.N 21/5:8/1178 Investigation of the operating properties of the leakage current anemometer / 1
Y 3.N 21/5:8/1179 Determination of the stress concentration factor of a stepped shaft stressed in torsion by means of precision strain gages / 1
Y 3.N 21/5:8/1180 Maintaining laminar flow in the boundary layer using a swept-back wing / 1
Y 3.N 21/5:8/1181 Investigations on reductions of friction on wings, in particular by means of boundary layer suction / 1
Y 3.N 21/5:8/1182 The problem of torsion in prismatic members of circular segmental cross section / 1
Y 3.N 21/5:8/1183 Temperatures and stresses on hollow blades for gas turbines / 1
Y 3.N 21/5:8/1184 Development and construction of an interferometer for optical measurements of density fields / 1
Y 3.N 21/5:8/1185 Systematic investigations of the influence of the shape of the profile upon the position of the transition point / 1
Y 3.N 21/5:8/1186 Comparison of drop and wind-tunnel experiments on bomb drag at high subsonic speeds / 1
Y 3.N 21/5:8/1187 Equations for adiabatic but rotational steady gas flows without friction / 1
Y 3.N 21/5:8/1188 The elasto-plastic stability of plates / 1
Y 3.N 21/5:8/1189 Theoretical analysis of stationary potential flows and boundary layers at high speed / 1
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