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- 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
- Investigation of the NiAl Phase of Nickel-Aluminum Alloys
- A Limited Correlation of Atmospheric Sounding Data and Turbulence Experienced by Rocket-Powered Models
- Investigation of the Low-Speed Flight Characteristics of a 1/15-Scale Model of the Convair XB-58 Airplane: Coord. No. AF-AM-15
- Investigation of the Influence of the Boundaries of a High-Speed Free Water Jet on the Planing Lift of a Flat Plate
- Experimental Investigation of Water Injection in Subsonic Diffuser of a Conical Inlet Operation at Free-Stream Mach Number of 2.5
- Experimental Hinge Moments on Two Freely Oscillating Trailing-Edge Controls Hinged at 55 Percent Control Chord
- Experimental Investigation of a Method of Wave-Drag Reduction for Combinations Employing Quasicylindrical Bodies and Swept Wings at Supersonic Speeds
- Effect of an Interface on Transient Temperature Distribution in Composite Aircraft Joints
- Impact-Loads Investigation of Chine-Immersed Model Having a Circular-Arc Transverse Shape
- Hydrogen for Turbojet and Ramjet Powered Flight
- Incompressible Flutter Characteristics of Representative Aircraft Wings
- Effect of Ground Proximity on Aerodynamic Characteristics of Two Horizontal-Attitude Jet Vertical-Take-Off-and-Landing Airplane Models
- Effect of Ground Proximity on the Aerodynamic Characteristics of a Four-Engine Vertical-Take-Off-and-Landing Transport-Airplane Model With Tilting Wing and Propellers
- Effect of Initial Mixture-Temperature on Burning Velocity of Hydrogen-Air Mixtures With Preheating and Simulated Preburning
- Pressure Drag of Axisymmetric Cowls Having Large Initial Lip Angles at Mach Numbers From 1.90 to 3.88