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- Some Measurements of Noise From Three Solid-Fuel Rocket Engines
- Turbulent-Heat-Transfer Measurements at a Mach Number of 3.03
- Theoretical Investigation at Subsonic Speeds of the Flow Ahead of a Slender Inclined Parabolic-Arc Body of Revolution and Correlation With Experimental Data Obtained at Low Speeds
- Elastic Buckling Under Combined Stresses of Flat Plates With Integral Waffle-Like Stiffening
- Burning Times of Magnesium Ribbons in Various Atmospheres
- Investigation of Lift, Drag, and Pitching Moment of a 60 Degrees Delta-Wind-Body Combination (AGARD Calibration Model B) in the Langley 9-Inch Supersonic Tunnel
- Lubricants of Reduced Flammability
- An Investigation of the Creep Lifetime of 75S-T6 Aluminum-Alloy Columns
- Initial Experiments on Flutter of Unswept Cantilever Wings at Mach Number 1.3
- Investigation of a Slat in Several Different Positions on an NACA 64A010 Airfoil for a Wide Range of Subsonic Mach Numbers
- The Free-Stream Boundaries of Turbulent Flows
- Experimental investigation of notch-size effects on rotating-beam fatigue behavior of 75S-T6 aluminum alloy
- Influence of Exposed Area on Stress-Corrosion Cracking of 24S Aluminum Alloy
- Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-Aspect-Ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane - Longitudinal Stability and Control
- Vertical Descent and Landing Tests of a 0.13-Scale Model of the Convair XFY-1 Vertically Rising Airplane in Still Air, TED No. NACA DE 368
- Preliminary Altitude Performance Data for the J65-B3 Turbojet Engine at Reynolds Number Indices from 0.2 to 0.8
- Performance and Boundary-Layer Data From 12 Degree and 23 Degree Conical Diffusers of Area Ratio 2.0 at Mach Numbers Up to Choking and Reynolds Numbers Up to 7.5 X 10(6)
- Performance of Air-Launched T-40 Rocket Motors with Two Types of Igniter
- Experiments on a Tail-Wheel Shimmy
- Static Longitudinal and Lateral Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane at a Mach Number of 1.41
- Additional Results on the Static Longitudinal and Lateral Stability Characteristics of a 0.05-Scale Model of the Convair F2Y-1 Airplane at High Subsonic Speeds
- Flight Determination of the Longitudinal Stability Characteristics of a 0.133-Scale Rocket-Powered Model of the Consolidated Vultee XFY-1 Airplane without Propellers at Mach Numbers from 0.73 to 1.19, TED No. NACA DE 369
- A Transonic Wind-Tunnel Investigation of the Longitudinal Aerodynamic Characteristics of a Model of the Lockheed XF-104 Airplane
- Hydrodynamic Investigation of the the Take-Off Characteristics of a 1/10-Scale Dynamic Model of the Convair XF2Y-1 Airplane
- A Thermal Equation for Flame Quenching
- Wind-Tunnel Tests of a Model of a Wingless Fin-Controlled Missile to Obtain Static Stability and Control Characteristics Through a Range of Mach Numbers From 0.5 to 0.88
- Papers on Shimmy and Rolling Behavior of Landing Gears Presented at Stuttgart Conference October 16 and 17, 1941
- Similar Solutions for the Compressible Laminar Boundary Layer with Heat Transfer and Pressure Gradient
- Charts Relating the Compressive Buckling Stress of Longitudinally Supported Plates to the Effective Deflectional and Rotational Stiffness of the Supports
- Ditching Investigation of a 1/10-Scale Model of the North American F-86 Airplane
- On the Sound Field of a Point-Shaped Sound Source in Uniform Translatory Motion
- Preliminary Altitude Operational Characteristics of a J57-P1 Turbojet Engine
- Flight Tests of a 0.13-Scale Model of the Convair XFY-1 Vertically Rising Airplane with the Lower Vertical Tail Removed, TED No. DE 368
- Experimental Determination of Linear Dynamics of Two-Spool Turbojet Engines
- Design and Evaluation of a Turbojet Exhaust Simulator, Utilizing a Solid-Propellant Rocket Motor, for Use in Free-Flight Aerodynamic Research Models
- Aerodynamic Characteristics of a Circular Cylinder at Mach Number 6.86 and Angles of Attack Up to 90 Degrees
- Average Skin-Friction Drag Coefficients From Tank Tests of a Parabolic Body of Revolution (NACA RM-10)
- Interim Report on Free-Spinning-Tunnel Investigation of a 1/25-Scale Model of the McDonnell F3H-1N Airplane, TED No. NACA AD 3100
- Flight Measurements of Average Skin-Friction Coefficients on a Parabolic Body of Revolution (NACA RM-10) at Mach Numbers from 1.0 to 3.7
- Longitudinal Stability and Control Characteristics at Transonic Speeds of a 1/30-Scale Model of the Republic XF-103 Airplane
- On Force-Deflection Diagrams of Airplane Shock Absorber Struts: First, Second, and Third Partial Reports
- Analysis of Turbulent Heat Transfer, Mass Transfer, and Friction in Smooth Tubes at High Prandtl and Schmidt Numbers
- Take-Off and Landing Characteristics of a 0.13-Scale Model of the Convair XFY-1 Vertically Rising Airplane in Steady Winds, TED No. NACA DE 368
- Supplementary Investigation in the Free-Spinning Tunnel of a 1/24-Scale Model of the Grumman F9F-6 Airplane Incorporating only Flaperons for Lateral Control, TED No. NACA DE 364
- Summary of Turbulence Data Obtained During United Air Lines Flight Evaluation of an Experimental C Band (5.5 cm) Airborne Weather Radar
- An Investigation in the Ames 40- by 80-Foot Wind Tunnel of a YT-56A Turboprop Engine Incorporating a Decoupler and a Controlled-Feathering Device
- Wind-Tunnel Investigation of the Effects on the Aerodynamic Characteristics of Modifications to a Model of a Bomb Mounted on a Wing-Fuselage Model and to a Model of the Bomb Alone
- Effect of Variable Viscosity and Thermal Conductivity on High-Speed Slip Flow Between Concentric Cylinders
- Drop Hammer Tests With Three Oleo Strut Models and Three Different Shock Strut Oils at Low Temperatures
- Effect of Rocket-Motor Operation on the Drag of Three 1/5-Scale Hermes A-3A Models in Free Flight