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- Deflection and Stress Analysis of Thin Solid Wings of Arbitrary Plan Form with Particular Reference to Delta Wings
- One-Dimensional Analysis of Choked-Flow Turbines
- Theoretical Prediction of Pressure Distributions on Nonlifting Airfoils at High Subsonic Speeds
- Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems: Effect of Missile Configuration on the Speed of Response
- A Method for Estimating the Rolling Moments Caused by Wing-Tail Interference for Missiles at Supersonic Speeds
- Investigation of Pressure Recovery of a Single-Conical-Shock Nose Inlet at Mach Number 5.4
- Weight Bar Charts
- Criticality Survey of Hydroxides as Coolant Moderators for Aircraft Nuclear Reactors
- Summary Report on Analytical Evaluation of Air and Fuel Specific-Impulse Characteristics of Several Nonhydrocarbon Jet-Engine Fuels
- Static Longitudinal Stability and Control Characteristics of a 1/16 -Scale Model of the Douglas D-558-II Research Airplane at Mach Numbers of 1.61 and 2.01
- Performance Characteristics of a Double-Cylindrical-Shroud Ejector Nozzle
- Wind-Tunnel Investigation of the Motion of a 1/10-Scale Model of the Douglas XF4D-1 Escape Capsule When Jettisoned by Jet Ejection: TED No. NACA DE 359
- The Low-Speed Lift and Drag Characteristics of a Series of Airplane Models Having Triangular or Modified Triangular Wings
- Damping in Pitch of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds
- Effect of Large Deflection of a Canard Control and Deflections of a Wing-Tip Control on the Static-Stability and Induced-Roll Characteristics of a Cruciform Canard Missile at a Mach Number of 2.01
- Effects of External Store Mounting on the Buffet, Trim, and Drag Characteristics of Rocket-Powered Fuselage and Store Combinations Between Mach Numbers of 0.7 and 1.4
- Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine 13: Endurance Evaluation of Several Protective Coatings Applied to Turbine Blades of Nonstrategic Steels
- Effects of Span and Spanwise and Chordwise Location on the Control Effectiveness of Spoilers on a 50 Degree Sweptback Wing at Mach Numbers of 1.41 and 1.96
- Equations, Tables, and Charts for Compressible Flow
- A Compilation of Summaries From NACA Reports on Fuels Research, 1945-1952
- Effect of Capture on the Slowing-Down Length of Neutrons in Hydrogenous Mixtures Containing Uranium
- Transonic Flow Past Cone Cylinders
- Investigation of an Axial-Flow-Compressor Rotor With Circular-Arc Blades Operating Up to a Rotor-Inlet Relative Mach Number of 1.22
- Preliminary Experiments with Pilot Burners for Ram-Jet Combustors
- Preliminary Investigation of the Effects of Cascading on the Oscillating Lift Force of an Airfoil Vibrated in Bending
- Supersonic Flow Past Oscillating Airfoils Including Nonlinear Thickness Effects
- Correlation by the Hypersonic Similarity Rule of the Pressure Distributions and Wave Drags for Minimum-Drag Nose Shapes at Zero Angle of Attack
- A Transonic Wind-Tunnel Investigation of the Effect of Modifications to an Indented Body in Combination With a 45 Degree Sweptback Wing
- A Transonic Wind-Tunnel Investigation of the Effects of Longitudinal Wing Location and Varying Body Size on the Interference Characteristics of a 45 Degrees Sweptback Wing
- Correlation of Flight and Wind-Tunnel Measurements of Roll-Off in Low-Speed Stalls on a 35 Degree Swept-Wing Aircraft
- Dynamic Characteristics of a Single-Spool Turbojet Engine
- Preliminary Results of an Investigation of the Effects of Spinner Shape on the Characteristics of an NACA D-Type Cowl Behind a Three-Blade Propeller, Including the Characteristics of the Propeller at Negative Thrust
- Transverse Vibrations of Hollow Thin-Walled Cylindrical Beams
- Investigation of Aerodynamic and Icing Characteristics of a Flush Alternate-Inlet Induction-System Air Scoop
- Altitude Investigation of Several Afterburner Configurations for the J40-WE-8 Turbojet Engine
- Experimental Investigation of the Aerodynamic Characteristics of an Air-to-Air Missile Employing Cruciform Wings and Tail of Rectangular Plan Form at Mach Numbers of 1.4 and 1.9
- Comparison of Calculated and Measured Thermal Distortions in a Reactor Control Rod for Temperature Patterns Simulating Two Reactor Operating Conditions
- Performance of a Normal-Shock Scoop Inlet with Boundary-Layer Control
- The Synthesis of Butylsilanes by a Large-Scale Reduction with Lithium Aluminum Hydride
- Control Hinge-Moment and Effectiveness Characteristics of a Horn-Balanced, Flap-Type Control on a 55 Degree Sweptback Triangular Wing of Aspect Ratio 3.5 at Mach Numbers of 1.41, 1.62, and 1.96
- Tests of the NACA 0010-1.50 40/1.051 Airfoil Section at High Subsonic Mach Numbers
- The Sodium Hydroxide Reactor - Effect of Reactor Variables on Criticality and Fuel- Element Temperature Requirements for Subsonic and Supersonic Aircraft Nuclear Propulsion
- Preliminary Results of Heat Transfer from a Stationary and Rotating Ellipsoidal Spinner
- Stability and Control Characteristics at High Subsonic Speeds of a 1/30-Scale Model of the MX-1554A Design
- Stability and Control Characteristics at Low Speed of a Modified 1/10-Scale Model of the MX-1554A Design
- Stability and Control Characteristics at Low Speed of a 1/10-Scale Model of MX-1554A Design
- An Investigation of the Dynamic and Static Stability Characteristics of a Group of Specialized Store Configurations at Transonic Speeds
- Transonic Aerodynamic and Trim Characteristics of 1/15-Scale Models of the Convair MX-1964 Airplane With Indented Fuselage
- Results of a Power-on Flight of a 1/10-Scale Rocket-Propelled Model of the Convair XF2Y-1 Airplane at a Mach Number of 1.53
- Theoretical Performance of Liquid Hydrogen and Liquid Fluorine as a Rocket Propellant