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- Effect of fuselage fences on the angle-of-attack supersonic performance of a top-inlet-fuselage configuration
- A theoretical analysis of the effect of engine angular momentum on longitudinal and directional stability in steady rolling maneuvers
- An experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface
- Gust-load and airspeed data from one type of four-engine airplane on five routes from 1947 to 1954
- Free-flight investigation to determine some effects of tail damping and wing-tail interference on the rolling effectiveness of inboard and outboard ailerons on an untapered sweptback wing
- Free-flight investigation, including some effects of wing aeroelasticity, of the rolling effectiveness of an all-movable horizontal tail with differential incidence at Mach numbers from 0.6 to 1.5
- Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303
- Development of a new flutter testing technique using a towed dynamic airplane model equipped with an automatic stabilizing system: Experimental and calculated dynamic stability characteristics for speeds up to 200 mph
- A survey of unclassified axial-flow-compressor literature
- Flight measurements of the vertical-tail loads on the Convair XF-92A delta-wing airplane
- Effects of sweep and taper on the longitudinal characteristics of an aspect ratio 3 wing-body combination at Mach numbers from 0.6 to 1.4
- A method for simulating the atmospheric entry of long-range ballistic missiles
- Flight Determination of the Longitudinal Stability and Control Characteristics of a 0.125-Scale Rocket-Boosted Model of the Mcdonnell F-101 Airplane at Mach Numbers from 0.82 to 1.84
- An investigation of string support interference on base pressure and forebody chord force at Mach numbers from 0.60 to 1.30
- Collection and summary of flap-type-aileron rolling-effectiveness data at zero lift as determined by rocket-powered model tests at Mach numbers between 0.6 and 1.6
- The longitudinal characteristics at Mach numbers up to 0.92 of several wing-fuselage-tail combinations having sweptback wings with NACA four-digit thickness distributions
- The effect of wing height on the longitudinal characteristics at high subsonic speeds of a wing-fuselage-tail combination having a wing with 40 degrees of sweepback and NACA four digit thickness distribution
- Icing Limit and Wet-Surface Temperature Variation for Two Airfoil Shapes Under Simulated High-Speed Flight Conditions
- A Fibrous-Glass Compact as a Permeable Material for Boundary-Layer-Control Applications Using Area Suction
- A Heated-Wire Liquid-Water-Content Instrument and Results of Initial Flight Tests in Icing Conditions
- Quasi-Cylindrical Theory of Wing-Body Interfernece at Supersonic Speeds and Comparison With Experiment
- Some Measurements of Flow in a Rectangular Cutout
- Simplified Procedures and Charts for the Rapid Estimation of Bending Frequencies of Rotating Beams
- Response of Homogeneous and Two-Material Laminated Cylinders to Sinusoidal Environmental Temperature Change, With Applications to Hot-Wire Anemometry and Thermocouple Pyrometry
- Effect of Dissociation on Thermodynamic Properties of Pure Diatomic Gases
- Cooperative Investigation of Relationship Between Static and Fatigue Properties of Wrought N-155 Alloy at Elevated Temperatures
- Shearing Effectiveness of Integral Stiffening
- Effect of Pressure on Thermal Conductance of Contact Joints
- Separation, Stability, and Other Properties of Compressible Laminar Boundary Layer With Pressure Gradient and Heat Transfer
- Unstable Convection in Vertical Channels With Heating From Below, Including Effects of Heat Sources and Frictional Heating
- A Universal Column Formula for Load at Which Yielding Starts
- A Polar-Coordinate Survey Method for Determining Jet-Engine Combustion-Chamber Performance
- Plastic Deformation of Aluminum Single Crystals at Elevated Temperatures
- Investigation of the Turbulent Boundary Layer on a Yawed Flat Plate
- Investigation of the Use of a Rubber Analog in the Study of Stress Distribution in Riveted and Cemented Joints
- The Linearized Equations of Motion Underlying the Dynamic Stability of Aircraft, Spinning Projectiles, and Symmetrical Missiles
- Cumulative Fatigue Damage of Axially Loaded Alclad 75S-T6 and Alclad 24S-T3 Aluminum-Alloy Sheet
- Effect of a Discontinuity on Turbulent Boundary-Layer-Thickness Parameters With Application to Shock-Induced Separation
- Effect of Interaction on Landing-Gear Behavior and Dynamic Loads in a Flexible Airplane Structure
- Pressure Waves Generated by Addition of Heat in a Gaseous Medium
- Averaging of Periodic Pressure Pulsations by a Total-Pressure Probe
- Theory of the Jet Syphon
- Some Considerations on Two-Dimensional Thin Airfoils Deforming in Supersonic Flow
- Laminar Boundary Layer Behind Shock Advancing Into Stationary Fluid
- Laboratory Investigation of an Autopilot Utilizing a Mechanical Linkage With a Dead Spot to Obtain an Effective Rate Signal
- Laminar Free Convection on a Vertical Plate With Prescribed Nonuniform Wall Heat Flux or Prescribed Nonuniform Wall Temperature
- Theoretical Analyses to Determine Unbalanced Trailing-Edge Controls Having Minimum Hinge Moments Due to Deflection at Supersonic Speeds
- A Thermal Equation for Flame Quenching
- Maximum Theorems and Reflections of Simple Waves
- A Theoretical Analysis of the Field of Random Noise Source Above an Infinite Plane