Browse TRAIL Inventories

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


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