Call Number (LC) Title Results
Y 3.N 21/5:8/1293 Approximate method of integration of laminar boundary layer in incompressible fluid / 1
Y 3.N 21/5:8/1294 Exhaust turbine and jet propulsion systems / 1
Y 3.N 21/5:8/1295 Gas flow with straight transition line / 1
Y 3.N 21/5:8/1296 On the theory of combustion of initially unmixed gases / 1
Y 3.N 21/5:8/1297 State and development of flutter calculation / 1
Y 3.N 21/5:8/1298 On the problem of gas flow over an infinite cascade using Chaplygin's approximation / 1
Y 3.N 21/5:8/1299 Additional measurements of the drag of surface irregularities in turbulent boundary layers / 1
Y 3.N 21/5:8/1300 Wind-tunnel corrections at high subsonic speeds particularly for an enclosed circular tunnel / 1
Y 3.N 21/5:8/1301 The flow of gases in narrow channels / 1
Y 3.N 21/5:8/1302 Stability of the cylindrical shell of variable curvature / 1
Y 3.N 21/5:8/1303 Resistance of cascade of airfoils in gas stream at subsonic velocity / 1
Y 3.N 21/5:8/1304 Generalization of Joukowski formula to an airfoil of a cascade in compressible gas stream with subsonic velocities / 1
Y 3.N 21/5:8/1305 On ionization and luminescence in flames / 1
Y 3.N 21/5:8/1306 Three papers from conference on "Wing and tail-surface oscillations" - March 6-8, 1941, Munich / 1
Y 3.N 21/5:8/1307 Lateral control by spoilers at the DVL / 1
Y 3.N 21/5:8/1308 On motion of fluid in boundary layer near line of intersection of two planes / 1
Y 3.N 21/5:8/1309 On the theory of thin and thin-walled rods / 1
Y 3.N 21/5:8/1310 Correction factors for wind tunnels of elliptic section with partly open and partly closed test section / 1
Y 3.N 21/5:8/1311 Contributions to the theory of the spreading of a free jet issuing from a nozzle / 1
Y 3.N 21/5:8/1312 Calculation of the bending stresses in helicopter rotor blades / 1