Call Number (LC) Title Results
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
Y 3.N 21/5:8/1212 On the theory of the Laval nozzle / 1
Y 3.N 21/5:8/1213 Gas motion in a local supersonic region and conditions of potential-flow breakdown / 1
Y 3.N 21/5:8/1214 Jet diffusion in proximity of a wall / 1
Y 3.N 21/5:8/1215 Flow pattern in a converging-diverging nozzle / 1
Y 3.N 21/5:8/1216 An approximate method for calculation of the laminar boundary layer with suction for bodies of arbitrary shape / 1
Y 3.N 21/5:8/1217 Lecture series "Boundary layer theory". : Part 1 - Laminar flows / 1
Y 3.N 21/5:8/1218 Lecture series "Boundary layer theory". : Part 2 - Turbulent flows / 1
Y 3.N 21/5:8/1219 The influence of the application of power during spin recovery of multiengine airplanes / 1
Y 3.N 21/5:8/1220 Pressure-distribution measurements on the tail surfaces of a rotating model of the design BFW-M 31 / 1
Y 3.N 21/5:8/1221 Experimental flights for testing of a reactor as an expedient for the termination of dangerous spins / 1
Y 3.N 21/5:8/1222 Investigation of the model ME 210 in the spin wind tunnel of the DVL. : Fourth partial report - Model with long fuselage and with a vee tail / 1
Y 3.N 21/5:8/1223 Some experiences regarding the nonlinearity of hot wires / 1
Y 3.N 21/5:8/1224 Lame's wave functions of the ellipsoid of revolution / 1
Y 3.N 21/5:8/1225 Test report on three- and six-component measurements on a series of tapered wings of small aspect ratio. : (Partial Report: Trapezoidal wing) / 1