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- A simplified method for assessing the effect of steady rolling on angle of attack and sideslip
- A theoretical and experimental study of planing surfaces including effects of cross section and plan form
- On possible similarity solutions for three-dimensional incompressible laminar boundary layers 3: similarity with respect to stationary polar coordinates for small angle variation
- An investigation at low speed of the flow over a simulated flat plate at small angles of attack using pitot-static and hot-wire probes
- A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry
- Cascade investigation of a related series of 6-percent-thick guide-vane profiles and design charts
- Basic performance characteristics of several subsonic-diffuser-bypass-duct combinations for use with supersonic inlets
- Two-dimensional cascade tests of NACA 65-(C(sub zeta)(sub o))A(sub 10))10 blade sections at typical compressor hub conditions for speeds up to choking
- Preliminary investigation of dynamic lateral stability characteristics of a configuration of the North American X-15 research airplane
- Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute
- A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9
- Theoretical rocket performance of JP-4 fuel with mixtures of liquid ozone and fluorine
- Temperature measurements from a flight test of two wing-body combinations at 7 degree angle of attack for Mach numbers to 4.86 and Reynolds numbers to 19.2 X 10(exp 6)
- Investigation of the planing lift of a flat plate at speeds up to 170 feet per second
- Effect of bluntness on transition for a cone and a hollow cylinder at Mach 3.1
- Free-flight investigation of jet effect on the low-lift drag and longitudinal trim of a supersonic interceptor-type airplane configuration with an overhanging tail boom at Mach numbers from 1.09 to 1.34
- Experimental investigation of the forces and moments due to sideslip of a series of triangular vertical- and horizontal-tail combinations at Mach numbers of 1.62, 1.93, and 2.41
- Propellant vaporization as a criterion for rocket-engine design : experimental effect of fuel temperature on liquid-oxygen - heptane performance
- A study of injection processes for 15-percent fluorine - 85-percent oxygen and heptane in a 200-pound-thrust rocket engine
- Aerodynamic heating of a thin, unswept, untapered, multiweb, aluminum-alloy wing at Mach numbers up to 2.67 as determined from a free-flight investigation of a rocket-propelled model
- Performance of an experimental annular turbojet combustor with methane and propane
- Vertical force-deflection characteristics of a pair of 56-inch-diameter aircraft tires from static and drop tests with and without prerotation
- Investigation of the effects of propeller diameter on the ability of a flapped wing, with and without boundary-layer control, to deflect a propeller slipstream downward for vertical take-off
- Supplementary Investigation in the Langley 20-Foot Free-Spinning Tunnel of a 1/20-Scale Model of the Douglas F4D-1 Airplane With External Wing Fuel Tanks
- Effects of Extreme Surface Cooling on Boundary-Layer Transition
- Some Effects of Aileron Deflection on the Static Lateral and Directional Aerodynamic Characteristics of Four Contemporary Airplane Models
- Handbook of Structural Stability Part 2: Buckling of Composite Elements
- Relation of Currently Estimated ANP Performance to Required ANP Performance
- A Thermal System for Continuous Monitoring of Laminar and Turbulent Boundary-Layer Flows During Routine Flight
- Attenuation in a Shock Tube Due to Unsteady-Boundary-Layer Action
- The Mechanism of Thermal-Gradient Mass Transfer in the Sodium Hydroxide-Nickel System
- Far Noise Field of Air Jets and Jet Engines
- Full-Scale Investigation of Several Jet-Engine Noise-Reduction Nozzles
- Elliptic Cones Alone and with Wings at Supersonic Speed
- Growth of Disturbances in a Flame-Generated Shear Region
- Theoretical and Experimental Investigation of the Subsonic-Flow Fields Beneath Swept and Unswept Wings with Tables or Vortex-Induced Velocities
- Effect of Fatigue Crack on Static Strength: 2014-T6, 2024-T4, 6061-T6, 7075-T6 Open-Hole Monobloc Specimens
- Some Observations on Stress-Corrosion Cracking of Single Crystals of AZ61X Magnesium Alloy
- Some Factors Affecting the Static Longitudinal and Directional Stability Characteristics of Supersonic Aircraft Configurations
- Identification of Foreign Objects Damaging Compressor Blades in Turbojet Engines
- Propagation of Sound Into a Wind-Created Shadow Zone
- Further Experiments on the Stability of Laminar and Turbulent Hydrogen-Air Flames at Reduced Pressures
- Wind-Tunnel Flutter Tests at Mach Numbers Up to 3.0 of Boeing Wing Models for Weapons System 110A: Coord. No. AF-AM-108
- Statistical Approach to the Estimation of Loads and Pressures on Seaplane Hulls for Routine Operations
- Study of Some Burner Cross-Section Changes That Increase Space-Heating Rates
- Study of Pressure Distributions on Simple Sharp-Nosed Models at Mach Numbers From 16 to 18 in Helium Flow
- Summary of NACA Research on Ignition Lag of Self-Igniting Fuel - Nitric Acid Propellants
- Tables of Various Mach Number Functions for Specific-Heat Ratios From 1.28 to 1.38
- Appraisal of the Hazards of Friction-Spark Ignition of Aircraft Crash Fires
- Investigation of an Air-Cooled, Plug-Type, Variable-Area Exhaust Nozzle