Call Number (LC) Title Results
Y 3.N 21/5:8/1230 Effect of the acceleration of elongated bodies of revolution upon the resistance in a compressible flow / 1
Y 3.N 21/5:8/1231 Report on investigation of developed turbulence / 1
Y 3.N 21/5:8/1233 Contribution to the problem of flow at high speed / 1
Y 3.N 21/5:8/1234 Computation of thin-walled prismatic shells / 1
Y 3.N 21/5:8/1235 Investigation of conditions of titanium carbonization - IV / 1
Y 3.N 21/5:8/1236 A class of de Laval nozzles / 1
Y 3.N 21/5:8/1237 On the motions of an oscillating system under the influence of flip-flop controls / 1
Y 3.N 21/5:8/1238 Two-dimensional wing theory in the supersonic range / 1
Y 3.N 21/5:8/1239 Two-dimensional motion of a gas at large supersonic velocities / 1
Y 3.N 21/5:8/1240 Airfoil measurements in the DVL high-speed wind tunnel (2.7-meter diameter) / 1
Y 3.N 21/5:8/1241 Basic differential equations in general theory of elastic shells / 1
Y 3.N 21/5:8/1242 Theory of characteristics / 1
Y 3.N 21/5:8/1243 Two-dimensional potential flows / 1
Y 3.N 21/5:8/1244 Rotationally symmetric potential flows / 1
Y 3.N 21/5:8/1245 Lift force of an arrow-shaped wing / 1
Y 3.N 21/5:8/1246 Hydrodynamic properties of planing surfaces and flying boats / 1
Y 3.N 21/5:8/1247 Landing procedure in model ditching tests of Bf 109 / 1
Y 3.N 21/5:8/1248 Investigations of lateral stability of a glide bomb using automatic control having no time lag / 1
Y 3.N 21/5:8/1249 Susceptibility to welding cracking, welding sensitivity, susceptibility to welding seam cracking, and test methods for these failures /
On a class of exact solutions of the equations of motion of a viscous fluid / 		2
Y 3.N 21/5:8/1250 Subsonic gas flow past a wing profile / 1