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- Compressive buckling of flat rectangular metalite type sandwich plates with simply supported loaded edges and clamped unloaded edges
- Analysis of flow in a subsonic mixed-flow impeller
- Bonding of molybdenum disulfide to various materials to form a solid lubricating film II : friction and endurance characteristics of films bonded by practical methods
- Bonding of molybdenum disulfide to various materials to form a solid lubricating film I : the bonding mechanism
- Evaluation of three methods for determining dynamic characteristics of a turbojet engine
- Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections
- Effects of moderate biaxial stretch-forming on tensile and crazing properties of acrylic plastic glazing
- Effective lubrication range for steel surfaces boundary lubricated at high sliding velocities by various classes of synthetic fluids
- Estimate of slip effect on compressible laminar-boundary-layer skin friction
- Experimental investigation of heat transfer through laminar and turbulent boundary layers on a cooled flat plate at a mach number of 2.4
- An experimental investigation of the behavior of 24S-T4 aluminum alloy subjected to repeated stresses of constant and varying amplitudes
- Supersonic flow with whirl and vorticity in axisymmetric channels
- Simple graphical solution of heat transfer and evaporation from surface heated to prevent icing
- Span load distributions resulting from angle of attack, rolling, and pitching for tapered sweptback wings with streamwise tips
- Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips: Subsonic leading edges and supersonic trailing edges
- Relative importance of various sources of defect-producing hydrogen introduced into steel during application of vitreous coatings
- Section characteristics of a 10.5-percent-thick airfoil with area suction as affected by chordwise distribution of permeability
- Survey of the chromium-cobalt-nickel phase diagram at 1200 C
- Survey of portions of the cobalt-chromium-iron-nickel quaternary system
- Experimental studies of noise from subsonic jets in still air
- Effect of a finite trailing-edge thickness on the drag of rectangular and delta wings at supersonic speeds
- An approximate method for determining the displacement effects and viscous drag of laminar boundary layers in two-dimensional hypersonic flow
- Investigation of 75-millimeter-bore deep-groove ball bearings under radial load at high speeds 1: oil-flow-studies
- A theoretical and experimental investigation of the influence of temperature gradients on the deformation and burst speeds of rotating disks
- Theoretical augmentation of turbine-propeller engine by compressor-inlet water injection, tail-pipe burning, and their combination
- Summary of acceleration and airspeed data from commercial transport airplanes during the period from 1933 to 1945
- A summary of diagonal tension Part I : methods of analysis
- A summary of diagonal tension Part II : experimental evidence
- Thermal buckling of plates
- Altitude operational characteristics of a prototype model of the J47D (RX1-1 and RX1-3) turbojet engines with integrated electronic control
- Two-dimensional shear flow in a 90 degrees elbow
- Theoretical study of the transonic lift of a double-wedge profile with detached bow wave
- A solution of the Navier-Stokes equation for source and sink flows of a viscous heat-conducting compressible fluid
- Solutions of laminar-boundary-equations which result in specific-weight-flow profiles locally exceeding free-stream values
- Some dynamic effects of fuel motion in simplified model tip tanks on suddenly excited bending oscillations
- Some effects of amplitude and frequency on the aerodynamic damping of a model oscillating continuously in yaw
- An analysis of the errors in curve-fitting problems with an application to the calculation of stability parameters from flight data
- Effect of high-lift devices on the static-lateral-stability derivatives of a 45 degree sweptback wing of aspect ratio 4.0 and taper ratio 0.6 in combination with a body
- Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed
- Auxiliary equipment and techniques for adapting the constant-temperature hot-wire anemometer to specific problems in air-flow measurements
- An engineering method for estimating notch-size effect in fatigue tests on steel
- 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
- Influence of structure on properties of sintered chromium carbide
- Experimental investigation of the local and average skin friction in the laminar boundary layer on a flat plate at a Mach number of 2.4
- Experimental investigation of an NACA 64A010 airfoil section with 41 suction slots on each surface for control of laminar boundary layer
- Experimental study of the effects of finite surface disturbances and angle of attack on the laminar boundary layer of an NACA 64A010 airfoil with area suction
- Numerical determination of indicial lift and moment functions for a two-dimensional sinking and pitching airfoil at Mach numbers 0.5 and 0.6
- Method for calculation of heat transfer in laminar region of air flow around cylinders of arbitrary cross section (including large temperature differences and transpiration cooling)
- The planing characteristics of a surface having a basic angle of dead rise of 20 degrees and horizontal chine flare
- The planing characteristics of a surface having a basic angle of dead rise of 40 degrees and horizontal chine flare