Call Number (LC) Title Results
Y 3.N 21/5:6/2481 Hydrodynamic characteristics of a low-drag, planing-tail flying-boat hull / 1
Y 3.N 21/5:6/2482 Stability and control characteristics of a complete airplane model having a wing with quarter-chord line swept back 40 degrees, aspect ratio 2.50, and taper ratio 0.42 / 1
Y 3.N 21/5:6/2483 Effect of fuselage and tail surfaces on low-speed yawing characteristics of a swept-wing model as determined in curved-flow test section of Langley stability tunnel / 1
Y 3.N 21/5:6/2484 Effects of compressibility on the flow past a two-dimensional bump / 1
Y 3.N 21/5:6/2485 Pilot escape from spinning airplanes as determined from free-spinning-tunnel tests / 1
Y 3.N 21/5:6/2486 Theoretical characteristics of two-dimensional supersonic control surfaces / 1
Y 3.N 21/5:6/2487 Effect of ground interference on the aerodynamic characteristics of a 42 degree sweptback wing / 1
Y 3.N 21/5:6/2488 Wind-tunnel investigation of the contribution of a vertical tail to the directional stability of a fighter-type airplane / 1
Y 3.N 21/5:6/2489 Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes / 2
Y 3.N 21/5:6/2490 Flight investigation of some factors affecting the critical tail loads on large airplanes / 1
Y 3.N 21/5:6/2491 Kinetics of sintering chromium carbide / 1
Y 3.N 21/5:6/2492 A method of solving the direct and inverse problem of supersonic flow along arbitrary stream filaments of revolution in turbomachines / 1
Y 3.N 21/5:6/2493 Analysis of an axial compressor stage with infinitesimal and finite blade spacing / 1
Y 3.N 21/5:6/2494 Lift and moment on oscillating triangular and related wings with supersonic edges / 1
Y 3.N 21/5:6/2495 Wind-tunnel investigation of effects of various aerodynamic balance shapes and sweepback on control-surface characteristics of semispan tail surfaces with NACA 0009, 0015, 66-009, 66(215)-014, and circular-arc airfoil sections / 1
Y 3.N 21/5:6/2496 Flight investigation of a mechanical feel device in an irreversible elevator control system of a large airplane / 1
y 3.n 21/5:6/2497 Generalized conical-flow fields in supersonic wing theory / 1
Y 3.N 21/5:6/2498 Flight investigation of the effect of atmospheric turbulence on the climb performance of an airplane / 1
Y 3.N 21/5:6/2499 Laminar friction and heat transfer at Mach numbers from 1 to 10 / 1
Y 3.N 21/5:6/2500 A comparison of the turbulent boundary-layer growth on an unswept and a swept wing / 1