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- The attenuation characteristics of four specially designed mufflers tested on a practical engine setup
- Effect of high bulk temperatures on boundary lubrication of steel surfaces by synthetic fluids
- Calculations of upwash in the region above or below the wing-chord planes of swept-back wing-fuselage-nacelle combinations
- The effect of initial curvature on the strength of an inelastic column
- An analysis of the factors affecting the loss in lift and shift in aerodynamic center produced by the distortion of a swept wing under aerodynamic load
- Techniques for calculating parameters of nonlinear dynamic systems from response data
- A revised formula for the calculation of gust loads
- Structural efficiencies of various aluminum, titanium, and steel alloys at elevated temperatures
- Stresses around rectangular cutouts in torsion boxes
- An analysis of the power-off landing maneuver in terms of the capabilities of the pilot and the aerodynamic characteristics of the airplane
- Theoretical Performance Characteristics of Sharp Lip Inlets at Subsonic Speeds
- Theoretical pressure distribution and wave drags for conical boattails
- Flight measurements and analysis of helicopter normal load factors in maneuvers
- Impingement of water droplets on wedges and diamond airfoils at supersonic speeds
- Effects of finite span on the section characteristics of two 45 degree sweptback wings of aspect ratio 6
- Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignment of the rotor blade for zero angle of attack
- Application of a characteristic blade-to-blade solution to flow in a supersonic rotor with varying stream-filament thickness
- An application of the method of characteristics to two-dimensional transonic flows with detached shock waves
- Application of several methods for determining transfer functions and frequency response of aircraft from flight data
- Axial-load fatigue tests on notched and unnotched sheet specimens of 61S-T6 aluminum alloy, annealed 347 stainless steel, and heat-treated 403 stainless steel
- Drag of circular cylinders for a wide range of Reynolds numbers and Mach numbers
- Analysis of heat addition in a convergent-divergent nozzle
- Temperatures, thermal stress, and shock in heat-generating plates of constant conductivity and of conductivity that varies linearly with temperature
- Calculated spanwise lift distributions and aerodynamic influence coefficients for unswept wings in subsonic flow
- The calculation of pressure on slender airplanes in subsonic and supersonic flow
- A variable-frequency light synchronized with a high-speed motion-picture camera to provide very short exposure times
- Use of two-dimensional data in estimating loads on a 45 degree sweptback wing with slats and partial-span flaps
- Velocity potential and air forces associated with a triangular wing in supersonic flow, with subsonic leading edges, and deforming harmonically according to a general quadratic equation
- Effect of a Rapid Blade-Pitch Increase on the Thrust and Induced-Velocity Response of a Full-Scale Helicopter Rotor
- Electrostatic spark ignition-source hazard in airplane crashes
- The high-speed planing characteristics of a rectangular flat plate over a wide range of trim and wetted length
- Effect of thermal properties on laminar-boundary-layer characteristics
- Factors affecting laminar boundary layer measurements in a supersonic steam
- Direct-reading design charts for 24S-T3 aluminum-alloy flat compression panels having longitudinal formed hat-section stiffeners and comparisons with panels having z-section stiffeners
- Graphical solution of some automatic-control problems involving saturation effects with application to yaw dampers for aircraft
- Gust loads and operating airspeeds of one type of four-engine transport airplane on three routes from 1949 to 1953
- Coefficient of friction and damage to contact area during the early stages of fretting I : Glass, copper, or steel against copper
- A flight investigation of the effect of steady rolling on the natural frequencies of a body-tail combination
- Measurements of flying qualities of an F-47D-30 airplane to determine longitudinal stability and control and stalling characteristics
- Experimental investigation of two-dimensional tunnel-wall interference at high subsonic speeds
- Application of an electro-optical two-color pyrometer to measurement of flame temperature for liquid oxygen-hydrocarbon propellant combination
- Static force-deflection characteristics of six aircraft tires under combined loading
- Drag and Longitudinal Trim at Low Lift of the North American YF-100A Airplane at Mach Numbers from 0.76 to 1.77 as Determined from the Flight Test of a 0.11-Scale Rocket Model
- Calibration of the Friez Aerovane, Wind Measuring Set AN/GMQ-11
- The Base Pressure at Supersonic Speeds on Two-Dimensional Airfoils and Bodies of Revolution (With and Without Fins) Having Turbulent Boundary Layers
- Rocket-Model Measurements of Zero-Lift Damping in Roll of the Bell MX-776 Missile at Mach Numbers from 0.6 to 1.56
- Investigation of a Half-Conical Scoop Inlet Mounted at Five Alternate Circumferential Locations Around a Circular Fuselage: Pressure-Recovery Results at a Mach Number 2.01
- Summary of Rocket-Model Tests at Zero Lift of the Northrop MX-775B Missile Configuration from Mach Numbers of 0.9 to 1.8
- Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96
- Performance of a 13-Stage Development Compressor for the J40-WE-24 Engine at Equivalent Speeds from 30 to 112 Percent of Design