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- Annual Report of the National Advisory Committee for Aeronautics (33rd). Administrative Report Including Technical Report Nos. 863 to 891
- Dynamic Response of Control Servo System Installed in NAES-Equipped SB2C-5 Airplane (BuAer No. 83135)
- Ditching Investigation of a 1/10-Scale Model of the Grumman F9F-2 Airplane, TED No. NACA DE 335
- Ditching Investigation of a 1/15-Scale Model of the Convair-Liner Airplane
- Ditching Investigation of a 1/14-Scale Model of the Northrop C-125 Airplane
- Investigation of the Spin and Recovery Characteristics of a 0.057-Scale Model of the Modified Chance Vought XF7U-1 Airplane. TED No. NACA DE 311
- Free-Spinning-Tunnel Investigation of a 1/24-Scale Model of the Grumman AF-2S, -2W Airplane
- Free-Spinning-Tunnel Investigation of a 1/30-Scale Model of the Grumman XF10F-1 Airplane
- Instrument for Measuring the Wall Shearing Stress of Turbulent Boundary Layers
- Investigations of Lateral Stability of a Glide Bomb Using Automatic Control Having No Time Lag
- Investigations of the Wall-Shearing Stress in Turbulent Boundary Layers
- An Investigation of the Longitudinal Characteristics of the MX-656 Configuration Using Rocket-Propelled Models Preliminary Results at Mach Numbers from 0.65 to 1.25
- Some Studies on the Flow of a Gas in the Region of Transition Through the Velocity of Sound
- Theoretical Investigations on the Efficiency and the Conditions for the Realization of Jet Engines
- Wind-Tunnel Investigation of a Full-Scale Model of the Hughes MX-904 Missile
- Investigation of Downwash, Sidewash, and Mach Number Distribution Behind a Rectangular Wing at a Mach Number of 2.41
- Free-Flight Investigation of the Static and Dynamic Longitudinal Stability Characteristics of 1/3.7-Scale Rocket-Powered Models of the Bell MX-776A
- Theoretical Investigation of a Proportional-Plus-Flicker Automatic Pilot
- Tests of the Northrop XSSM-A-3 Missile in the Ames 40- by 80-Foot Wind Tunnel: Wing Modifications
- High-Subsonic Performance Characteristics and Boundary-Layer Investigations of a 12 10-Inch-Inlet-Diameter Conical Diffuser
- Free-Space Oscillating Pressures Near the Tips of Rotating Propellers
- The Gas Kinetics of Very High Flight Speeds
- Positioning Investigation of Single Slotted Flaps on a 47.7 Degrees Sweptback Wing at Reynolds Numbers of 4.0 X 10(Exp 6) and 6.0 X 10(Exp 6)
- Preliminary Empirical Design Requirements for the Prevention of Tumbling of Airplanes Having No Horizontal Tails
- Generalization of Boundary-Layer Momentum-Integral Equations to Three-Dimensional Flows Including Those of Rotating System
- Damping in Roll of Rectangular Wings of Several Aspect Ratios and Naca 65a-Series Airfoil Sections of Several Thickness Ratios at Transonic and Supersonic Speeds as Determined With Rocket-Powered Models
- Investigation of the NACA 3-(3)(05)-05 Eight-Blade Dual-Rotating Propeller at Forward Mach Numbers to 0.925
- Investigation of the NACA 4-(4)(06)-057-45a and NACA 4-(4)(06)-57-45b Two-Blade Swept Propellers at Forward Mach Numbers to 0.925
- Flight Measurements of Base Pressure on Bodies of Revolution With and Without Simulated Rocket Chambers
- Evaluation of Several Adhesives and Processes for Bonding Sandwich Constructions of Aluminum Facings on Paper Honeycomb Core
- Aerodynamic Characteristics of Damping Screens
- Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section
- Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7
- The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel
- An analysis of base pressure at supersonic velocities and comparison with experiment
- Analysis of an induction blowdown supersonic tunnel
- Analysis for Control Application of Dynamic Characteristics of Turbojet Engine With Tail-Pipe Burning
- Investigation of Boundary-layer Control to Improve the Lift and Drag Characteristics of the NACA 65₂-415 Airfoil Section with Double Slotted and Plain Flaps
- Temperature distribution in internally heated walls of heat exchangers composed of noncircular flow passages
- Compressive strength of flanges
- X-Ray Diffraction by Bent Crystal Lamellae
- Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8
- Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range
- Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade
- Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88
- NACA VGH recorder
- An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47©� sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel
- Average Outside-Surface Heat-Transfer Coefficients and Velocity Distributions for Heated and Cooled Impulse Turbine Blades in Static Cascades
- Flight Performance of a Jet Power Plant, III, operating characteristics of a jet power plant as a function of altitude
- Strain-Gage Measurements of Buffeting Loads on a Jet-Powered Bomber Airplane