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- Matching Characteristics of J35-A-23 Compressor and Two-stage Turbine
- Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds: Triangular Wing of Aspect Ratio 2 with NACA 0005-63 Thickness Distribution, Cambered and Twisted for a Trapezoidal Span Load Distribution
- Investigation of Surge Characteristics of XJ34-WE-32 Turbojet Engine
- Ditching Investigation of a 1/24-Scale Model of the Douglas C-124 Airplane
- Flight Instrument for Measurement of Liquid-Water Content in Clouds at Temperatures Above and Below Freezing
- An Instrument Employing a Coronal Discharge for the Determination of Droplet-Size Distribution in Clouds
- Measurement of distortion in second experimental control rod for argonne naval reactor with constant transverse temperature gradient and uniform longitudinal temperature distribution
- X-Ray Diffraction Study of the Internal Structure of Supercooled Water
- Spark Ignition of Flowing Gases. 2: Effect of Electrode Parameters on Energy Required to Ignite a Propane-Air Mixture
- Theoretical Investigation of Submerged Inlets at Low Speeds
- Analysis of the Liquid-metal Turbojet Cycle for Propulsion of Nuclear Powered Aircraft
- Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine. 7: Rotor-Blade Fabrication Procedures
- Effectiveness of Thermal-Pneumatic Airfoil-Ice-Protection System
- Heat delivery in a compressible flow and applications to hot-wire anemometry
- Analytical method for determining performance of turbojet-engine tail-pipe heat exchangers
- Effect of an autopilot sensitive to yawing velocity on the lateral stability of a typical high-speed airplane
- Fluctuations in a spray formed by two impinging jets
- Further comparisons of theoretical and experimental lift and pressure distributions on airfoils in cascade at low-subsonic speed
- Fundamental effects of cold-working on creep properties of low-carbon N-155 alloy
- Infrared spectra of 59 dicyclic hydrocarbons
- Investigation of NACA 64,2-432 and 64,3-440 airfoil sections with boundary-layer control and an analytical study of their possible applications
- A method of designing turbomachine blades with a desirable thickness distribution for compressible flow along an arbitrary stream filament of revolution
- A method for the determination of the spanwise load distribution of a flexible swept wing at subsonic speeds
- Method of analysis for compressible flow arbitrary turbomachine blades on general surface of revolution
- Lift and moment on oscillating triangular and related wings with supersonic edges
- Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane
- Full-scale-tunnel investigation of the static-thrust performance of a coaxial helicopter rotor
- Friction at high sliding velocities of oxide films on steel surfaces boundary-lubricated with stearic-acid solutions
- Heat transfer to bodies in a high-speed rarefied-gas stream
- On the second-order tunnel-wall-constriction corrections in two-dimensional compressible flow
- On the use of coupled modal functions in flutter analysis
- On two-dimensional flow after a curved stationary shock (with special reference to the problem of detached shock waves)
- Effect of fuel immersion on laminated plastics
- A critical review of notch sensitivity in stress-rupture tests
- Criterions for condensation-free flow in supersonic tunnels
- Analytical evaluation of aerodynamic characteristics of turbines with nontwisted rotor blades
- Analysis of pure-bending flutter of a cantilever swept wing and its relation to bending-torsion flutter
- An analytical investigation of effect of high-lift flaps on take-off of light airplanes
- Bench-test investigation of the transient-response characteristics of several simulated airplanes incorporating an autopilot sensitive to yawing accelerations
- Effect of various parameters including Mach number on the single-degree-of-freedom flutter of a control surface in potential flow
- Effectiveness of ceramic coatings in reducing corrosion of five heat-resistant alloys by lead-bromide vapors
- The effect of rate of change of angle of attack on the maximum lift coefficient of a pursuit airplane
- An experimental determination of the critical bending moment of a box beam stiffened by posts
- An experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow
- Tables of exact laminar-boundary-layer solutions when the wall is porous and fluid properties are variable
- A procedure for calculating the development of turbulent boundary layers under the influence of adverse pressure gradients
- Some measurements of the effect of gaseous imperfections on the critical pressure ratio in air and the speed of sound in nitrogen
- A study of elastic and plastic stress concentration factors due to notches and fillets in flat plates
- Static and fatigue strengths of high-strength aluminum-alloy bolted joints
- A self-synchronizing stroboscopic Schlieren system for the study of unsteady air flows