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- Drag Tests of an NACA 65(215)-114, a = 1.0 Practical-Construction Airfoil Section Equipped with a 0.295-Airfoil-Chord Slotted Flap
- Stress-Strain and Elongation Graphs for Alclad Aluminum-Alloy 75S-T Sheet
- Lifting-Surface-Theory Aspect-Ratio Corrections to the Lift and Hinge-Moment Parameters for Full-Span Elevators on Horizontal Tail Surfaces
- A Metallurgical Investigation of Large Forged Discs of Low-Carbon N-155 Alloy
- A Study of Piston-Ring Friction
- Performance Tests of Wire Strain Gages 5: Error in Indicated Bending Strains in Thin Sheet Metal Due to Thickness and Rigidity of Gage
- Experimental Studies of the Knock-Limited Blending Characteristics of Aviation Fuels 2: Investigation of Leaded Paraffinic Fuels in an Air-Cooled Cylinder
- Effect of Geometric Dihedral on the Aerodynamic Characteristics of Two Isolated Vee-Tail Surfaces
- The Spot Welding of Dissimilar Aluminum Alloys in the 0.040-Inch Thickness
- The Spot Welding of Alclad 24S-T in Thicknesses of 0.064, 0.081, and 0.102 Inch
- A Study of Several Parameters Controlling the Trajectories of a Supersonic Antiaircraft Missile Powered With Solid- or Liquid-Fuel Rockets
- The Linear Perturbation Theory of Axially Symmetric Compressible Flow With Application to the Effect of Compressibility on the Pressure Coefficient at the Surface of a Body of Revolution
- General Treatment of Compressible Flow in Ejectors and Example of Its Application to Problem of Effect of Ejector Addition on Thrust of Jet-Propulsion Units
- Flight Investigation of Thrust Augmentation of a Turbojet Engine by Water-Alcohol Injection
- Preliminary Investigation of Effects of Gamma Radiation on Age-Hardening Rate of an Aluminum-Copper Alloy
- The Subsonic Aerodynamic Characteristics of Two Double-Wedge Airfoil Sections Suitable for Supersonic Flight
- Estimation of Range of Stability Derivatives for Current and Future Pilotless Aircraft
- A Device for Measuring Sonic Velocity and Compressor Mach Number
- Tests of Submerged Duct Installation on a Modified Airplane in the Ames 40- by 80-foot Wind Tunnel
- Estimate of Hull-Weight Change with Varying Length-Beam Ratio for Flying Boats
- Effect of Modifications to Induction System on Altitude Performance of V-1710-93 Engine 3: Use of Parabolic Rotating Guide Vanes and NACA Designed Auxiliary-Stage Inlet Elbow and Interstage Duct
- Frequency-Response Method for Determination of Dynamic Stability Characteristics of Airplanes With Automatic Controls
- Flight Investigation on a Fighter-Type Airplane of Factors Which Affect the Loads and Load Distributions on the Vertical Tail Surfaces During Rudder Kicks and Fishtails
- A Theoretical Investigation of Hydrodynamic Impact Loads on Scalloped-Bottom Seaplanes and Comparisons With Experiment
- Dislocation Theory of the Fatigue of Metals
- Coefficient of Friction, Oil Flow and Heat Balance of a Full-Journal Bearing
- Spark-Timing Control Based on Correlation of Maximum-Economy Spark Timing, Flame-Front Travel, and Cylinder-Pressure Rise
- On Similarity Rules for Transonic Flows
- The Development of Jet-Engine Nacelles for a High-Speed Bomber Design
- Calculations and Experimental Investigations on the Feed-Power Requirement of Airplanes With Boundary-Layer Control
- Analytical Treatment of Normal Condensation Shock
- Calibration and Measurement in Turbulence Research by the Hot-Wire Method
- The Combination of Internal-Combustion Engine and Gas Turbine
- Description of Russian Aircraft Engines "AM 35" and "AM 38"
- Development and Construction of an Interferometer for Optical Measurements of Density Fields
- Determination of the Stress Concentration Factor of a Stepped Shaft Stressed in Torsion by Means of Precision Strain Gages
- Concerning the Velocity of Evaporation of Small Droplets in a Gas Atmosphere
- Compressible Flow Tables for Air
- Cones in Supersonic Flow
- Compression Shocks of Detached Flow
- The Distribution of Loads on Rivets Connecting a Plate to a Beam Under Transverse Loads
- Drag Reduction by Suction of the Boundary Layer Separated Behind Shock Wave Formation at High Mach Numbers
- Force and Pressure-Distribution Measurements on a Rectangular Wing With a Slotted Droop Nose and With Either Plain and Split Flaps in Combination or a Slotted Flap
- Investigations on Reductions of Friction on Wings, in Particular by Means of Boundary Layer Suction
- NACA Conference on Aerodynamic Problems of Transonic Airplane Design
- A Method for Estimating Heat Requirements for Ice Prevention Gas Heated Hollow Propeller Blades
- Introduction to the Problem of Rocket-Powered Aircraft Performance
- Wind-tunnel investigation of the effect of tab balance on tab and control-surface characteristics
- The Performance of a Composite Engine Consisting of a Reciprocating Spark-Ignition Engine, a Blow-Down Turbine, and a Steady-Flow Turbine
- Experimental Studies of Knock-Limited Blending Characteristics of Aviation Fuels 3 - Aromatics and Cycloparaffins