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- Theoretical and Experimental Investigation of Random Gust Loads Part 2: Theoretical Formulation of Atmospheric Gust Response Problem
- Theoretical and Experimental Investigation of Random Gust Loads Part 1: Aerodynamic Transfer Function of a Simple Wing Configuration in Incompressible Flow
- Rough-Water Impact-Load Investigation of a Chine-Immersed V-Bottom Model Having a Dead-Rise Angle of 10 Degrees
- A Power-Series Solution for the Unsteady Laminar Boundary-Layer Flow in an Expansion Wave of Finite Width Moving Through a Gas Initially at Rest
- Stability Limits and Burning Velocities for Some Laminar and Turbulent Propane and Hydrogen Flames at Reduced Pressure
- Some Considerations of Hysteresis Effects on Tire Motion and Wheel Shimmy
- Stability of Laminar Boundary Layer Near a Stagnation Point Over an Impermeable Wall and a Wall Cooled by Normal Fluid Injection
- Physical and Chemical Properties of HEF-2 (NACA Fuel 56Z4)
- A Thermocouple Subcarrier Oscillator for Telemetering Temperatures From Pilotless Aircraft
- Approximate Calculation of the Compressible Turbulent Boundary Layer With Heat Transfer and Arbitrary Pressure Gradient
- A Thermal System for Continuous Monitoring of Laminar and Turbulent Boundary-Layer Flows During Routine Flight
- A Study of The "Toss Factor" in the Impact Testing of Cermets by the Izod Pendulum Test
- A Study of the Impact Behavior of High-Temperature Materials
- A Discussion of Cone and Flat-Plate Reynolds Numbers for Equal Ratios of the Laminar Shear to the Shear Caused by Small Velocity Fluctuations in a Laminar Boundary Layer
- An Investigation of the Control Effectiveness of Tip Ailerons and Spoilers on a Low-Aspect-Ratio Trapezoidal-Wing Airplane Model at Mach Numbers From 1.55 to 2.35
- Free-Flight Investigation of the Drag of a Model of a 60 Degree Delta-Wing Bomber With Strut-Mounted Siamese Nacelles and Indented Fuselage at Mach Numbers From 0.80 to 1.35
- Spontaneous Flammability of Pentaborane and Pentaborane-3-Methylpentane Blends
- Handbook of Structural Stability Part 4: Failure of Plates and Composite Elements
- Handbook of Structural Stability Part 1: Buckling of Flat Plates
- Handbook of Structural Stability Part 5: Compressive Strength of Flat Stiffened Panels
- Handbook of Structural Stability Part 2: Buckling of Composite Elements
- Reduction of Oxidized Nichrome V Powders and Sintering of Nichrome V Bodies
- Handbook of Structural Stability Part 3: Buckling of Curved Plates and Shells
- Investigation at High Subsonic Speeds of the Use of Low Auxiliary Tail Surfaces Having Dihedral to Improve the Longitudinal and Directional Stability of a T-Tail Model at High Lift
- Laminar Boundary Layer With Heat Transfer on a Cone at Angle of Attack in a Supersonic Stream
- Thermal Decomposition of Some Group I, II, and III Metal Alkyls
- On Subsonic Flow Past a Paraboloid of Revolution
- Thermal Stability of a Commercial Propyl Pentaborane (HEF-2) in the Range 147 to 190 Degrees C
- Experimental Investigation of Transpiration Cooling for a Turbulent Boundary Layer in Subsonic Flow Using Air as a Coolant
- The Sine-Cosine Method for Reducing the Interference Pressure Drag of Sweptback Wings
- Full-Scale Investigation of Several Jet-Engine Noise-Reduction Nozzles
- Summary of 65-Series Compressor-Blade Low-Speed Cascade Data by Use of the Carpet-Plotting Technique
- The Mechanism of Thermal-Gradient Mass Transfer in the Sodium Hydroxide-Nickel System
- An Experimental Study at High Subsonic Speeds of Several Tail Configurations on a Model Having a 45 Degree Sweptback Wing
- Investigation at High Subsonic Speeds of the Effects of Various Horizontal Fuselage Forebody Fins on the Directional and Longitudinal Stability of a Complete Model Having a 45 Degree Sweptback Wing
- The Similarity Rules for Second-Order Subsonic and Supersonic Flow
- Sidewash in the Vicinity of Lifting Swept Wings at Supersonic Speeds
- Internal Performance of Two-Dimensional Wedge Exhaust Nozzles
- On Stokes' Stream Function in Compressible Small-Disturbance Theory
- Flight Investigation of the Low-Speed Characteristics of a 35 Degree Swept-Wing Airplane Equipped with an Area-Suction Ejector Flap and Various Wing Leading-Edge Devices
- Compressive Stress-Strain Properties of 17-7 PH and AM 350 Stainless-Steel Sheet at Elevated Temperatures
- Elliptic Cones Alone and with Wings at Supersonic Speeds
- Effects of Horizontal-Tail Position and a Wing Leading-Edge Modification Consisting of a Full-Span Flap and a Partial-Span Chord-Extension on the Aerodynamic Characteristics in Pitch at High Subsonic Speeds of a Model With a 45 Degree Sweptback Wing
- Investigation of Some Mechanical Properties of Thermenol Compressor Blades
- Experimental Investigation of Temperature Feedback Control Systems Applicable to Turbojet-Engine Control
- Experimental Comparison of Speed: Fuel-Flow and Speed-Area Controls on a Turbojet Engine for Small Step Disturbances
- Flight Investigation of the Transonic Longitudinal and Lateral Handling Qualities of the Douglas X-3 Research Airplane
- Investigation at Mach Numbers to 1.04 of Blade-Loading Characteristics of Two Full-Scale Three-Blade Supersonic Propellers Differing in Blade-Section Camber
- Tables of Characteristic Functions for Solving Boundary-Value Problems of the Wave Equation with Application to Supersonic Interference
- Effects of Some Configuration Changes on Afterburner Combustion Performance
