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- Plastic Stress-Strain Relations for 75S-T6 Aluminum Alloy Subjected to Biaxial Tensile Stresses
- A Multiple-Range Self-Balancing Thermocouple Potentiometer
- An Investigation of Aircraft Heaters 35: Thermocouple Conduction Error Observed in Measuring Surface Temperatures
- Forced-Convection Heat Transfer to Water at High Pressures and Temperatures in the Nonboiling Region
- Effect of Surface Finish on Fatigue Properties at Elevated Temperatures 1: Low-Carbon N-155 With Grain Size of A.S.T.M. 1
- Preliminary Investigation of Helmholtz Resonators for Damping Pressure Fluctuations in 3.6-Inch Ram Jet at Mach Number 1.90
- Theoretical and Experimental Investigation of Additive Drag
- Thermal Conductivity of 14 Metals and Alloys Up to 1100 Degrees Fahrenheit
- Properties of Low-Carbon N-155 Alloy Bar Stock From 1200 to 1800 Degrees Fahrenheit
- Experimental Investigation of Effect of Jet Exit Configuration on Thrust and Drag
- Altitude Wind Tunnel Investigation of the Performance of Compressor, Combustor, and Turbine Components of Prototype J47D (RX1-1) Turbojet Engine
- An Experimental Study of Water-Pressure Distributions During Landings and Planing of a Heavily Loaded Rectangular Flat-Plate Model
- Comparison of Measured Efficiencies of Nine Turbine Designs with Efficiencies Predicted by Two Empirical Methods
- Effective Modulus in Plastic Buckling of High-Strength Aluminum-Alloy Sheet
- An Investigation of the Low-Speed Stability and Control Characteristics of a 1/10-Scale Model of the McDonnell XF3H-1 Airplane: TED No. NACA DE 344
- Preliminary Investigation of Cooling-Air Ejector Performance at Pressure Ratios from 1 to 10
- Stability and Control Measurements Obtained during USAF-NACA Cooperative Flight-Test Program on the X-4 Airplane (USAF No. 46-677)
- Free-Spinning Tunnel Investigation of a 1/20-Scale Model of the McDonnell F2H-3 Airplane
- Low-Speed Characteristics of a 45 Degree Swept Wing with Leading-Edge Inlets
- Free-Spinning-Tunnel Investigation to Determine the Effect of Two Nose Designs on Spin and Recovery Characteristics of a 1/20-Scale Model of the McDonnel XF3H-1 Airplane: TED No. NACA DE 343
- Arrangement of Bodies of Revolution in Supersonic Flow to Reduce Wave Drag
- Analytical Investigation of Fully Developed Laminar Flow in Tubes With Heat Transfer With Fluid Properties Variable Along the Radius
- Wind-Tunnel Investigation of the Descent Characteristics of Bodies of Revolution Simulating Anti-Personnel Bombs
- Experimental Values of the Surface Tension of Supercooled Water
- An Empirical Method Permitting Rapid Determination of the Area, Rate and Distribution of Water-Drop Impingement on an Airfoil of Arbitrary Section at Subsonic Speeds
- Empirical Relation Between Induced Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind-Tunnel Tests on Four Model Rotors
- Determination of Shapes of Boattail Bodies of Revolution for Minimum Wave Drag
- Lateral-Control Characteristics and Dihedral Effect of a Wing-Body Combination With a Variable-Incidence Triangular Wing and Wing-Tip Ailerons at a Mach Number of 1.52
- NACA Investigations of Icing-Protection Systems for Turbojet-Engine Installations
- Method for Estimating Lift Interference of Wing-Body Combinations at Supersonic Speeds
- Calculated Performance of a Mercury-Compressor-Jet Powered Airplane Using a Nuclear Reactor as an Energy Source
- Analysis of Meteorological Data Obtained During Flight in a Supercooled Stratiform Cloud of High Liquid-Water Content
- Adaptation of a Cascade Impactor to Flight Measurement of Droplet Size in Clouds
- An Investigation of the Low-Speed Stability and Control Characteristics of a 1/10-Scale Model of the McDonnell XF3H-1 Airplane
- Meteorological Analysis of Icing Conditions Encountered in Low-Altitude Stratiform Clouds
- A General Correlation of Temperature Profiles Downstream of a Heated-Air Jet Directed Perpendicularly to an Air Stream
- Analysis of the Liquid-Metal Turbojet Cycle for Propulsion of Nuclear Powered Aircraft
- Pitching-Moment Derivatives Cmq and Cma at Supersonic Speeds for a Slender-Delta-Wing and Slender-Body Combination and Approximate Solutions for Broad-Delta-Wing and Slender-Body Combinations
- Possible Application of Blade Boundary-Layer Control to Improvement of Design and Off-Design Performance of Axial-Flow Turbomachines
- Practical Methods of Calculation Involved in the Experimental Study of an Autopilot and the Autopilot-Aircraft Combination
- A Photoelastic Investigation of Stress Concentrations Due to Small Fillets and Grooves in Tension
- Torsional Strength of Stiffened D-Tubes
- Turbulence-Intensity Measurements in a Jet of Air Issuing From a Long Tube
- Water-Landing Investigation of a Model Having Heavy Beam Loadings and 0 Degrees Angle of Dead Rise
- Flow Separation Ahead of Blunt Bodies at Supersonic Speeds
- An Investigation by the Hodograph Method of Flow Through a Symmetrical Nozzle With Locally Supersonic Regions
- Experimental Investigation of Localized Regions of Laminar-Boundary-Layer Separation
- An Investigation of Aircraft Heaters 37: Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Along a Flat Plate Containing Turbulence Promotors
- An Investigation of Aircraft Heaters 34: Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Between a Flat and a Wave-Shaped Plate
- An investigation of aircraft heaters 36: preliminary investigation of a combustion-type aircraft heater