Call Number (LC) Title Results
Y 3.N 21/5:6/2632 Corrosion of magnesium alloy ZK60A in marine atmosphere and tidewater / 1
Y 3.N 21/5:6/2633 Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers / 1
Y 3.N 21/5:6/2634 Evaluation of three methods for determining dynamic characteristics of a turbojet engine / 1
Y 3.N 21/5:6/2635 An analysis of laminar free-convection flow and heat transfer about a flat plate parallel to the direction of the generating body force / 1
Y 3.N 21/5:6/2636 Influence of lubricant viscosity on operating temperatures of 75-millimeter-bore cylindrical-roller bearing at high speeds / 1
Y 3.N 21/5:6/2637 Compressive buckling of flat rectangular Metalite type sandwich plates with simply supported loaded edges and clamped unloaded edges (Revised) / 1
Y 3.N 21/5:6/2638 Study of inadvertent speed increases in transport operation / 1
Y 3.N 21/5:6/2639 Fatigue strengths of aircraft materials. : Axial-load fatigue tests on notched sheet specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel with stress-concentration factor of 1.5 / 1
Y 3.N 21/5:6/2640 Interaction of column and local buckling in compression members / 1
Y 3.N 21/5:6/2641 A vector study of linearized supersonic flow applications to nonplanar problems / 1
Y 3.N 21/5:6/2642 Application of linear analysis to an experimental investigation of a turbojet engine with proportional speed control / 1
Y 3.N 21/5:6/2643 Span load distributions resulting from angle of attack, rolling, and pitching for tapered sweptback wings with streamwise tips. : Supersonic leading and trailing edges / 1
Y 3.N 21/5:6/2644 Experimental investigation of an NACA 64A010 airfoil section with 41 suction slots on each surface for control of laminar boundary layer / 1
Y 3.N 21/5:6/2645 Effects of wing lift and weight on landing-gear loads / 1
Y 3.N 21/5:6/2646 Inviscid flow about airfoils at high supersonic speeds / 1
Y 3.N 21/5:6/2647 Implication of the transport equation for the semiempirical treatment of shields / 1
Y 3.N 21/5:6/2648 Experimental investigation of transition of a model helicopter rotor from hovering to vertical autorotation / 1
Y 3.N 21/5:6/2649 Effect of Mach number on the flow and application of compressibility corrections in a two-dimensional subsonic-transonic compressor cascade having varied porous-wall suction at the blade tips / 1
Y 3.N 21/5:6/2650 Radioautographic method for examining distribution of particles in a cyclotron beam / 1
Y 3.N 21/5:6/2651 Supersonic conical flow / 1