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- 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
- A study of the transient behavior of shock waves in transonic channels flows
- Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers
- Analytical and experimental investigation of fully developed turbulent flow of air in a smooth tube with heat transfer with variable fluid properties
- Transonic similarity rules for lifting wings
- Use of the boundary layer of a cone to measure supersonic flow inclination
- An analysis of the normal accelerations and airspeeds of a two-engine type of transport airplane in commercial operations on routes in the central United States from 1948 to 1950
- A theory and method for applying interferometry to the measurement of certain two-dimensional gaseous density fields
- Wear and sliding friction properties of nickel alloys suited for cages of high-temperature rolling-contact bearings II : alloys retaining mechanical properties above 600 F
- The effects of Reynolds number on the application of NACA 16-series airfoil characteristics to propeller design
- A flight investigation of the effect of shape and thickness of the boundary layer on the pressure distribution in the presence of shock
- Experimental investigation of a 90 degree cascade diffusing bend with an area ratio of 1.45:1 and with several inlet boundary layers
- Orientation of orifices on bodies of revolution for determination of stream static pressure at supersonic speeds
- Comparison of supersonic minimum-drag airfoils determined by linear and nonlinear theory
- Comparison of two- and three-dimensional potential-flow solutions in a rotating impeller passage
- Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect ratio 4 and taper ratio 0.6