Browse TRAIL Inventories

Effects of the Lateral Oscillation of Fixing the Rudder and Reflexing the Flaps on the Bell X-1 Airplane

Exploratory Investigation of the Effect of Skewed Plain Nose Flaps on the Low-Speed Characteristics of a Large-Scale Triangular-Wing-Fuselage Model

Low-Speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface

Effect of an End Plate on the Aerodynamic Characteristics of a 20.55 Degree Sweptback Wing with an Aspect Ratio of 2.67 and a Taper Ratio of 0.5.: Transonic-Bump Method

Determination of Minimum Moments of Inertia of Arbitrarily Shaped Areas, Such as Hollow Turbine Blades

Lateral-Control Investigation at a Reynolds Number of 5,300,000 of a Wing of Aspect Ratio 5.8 Sweptforward 32 Degrees at the Leading Edge

High-Speed Aerodynamic Characteristics of a Lateral-Control Model 2: Modified NACA 0012-64 Section with a 26.6-Percent-Chord, Plain, Trailing-Edge Aileron; Wing Unswept and Swept Back 45 Degrees

Calculated Performance of Nuclear Turbojet Powered Airplane at Flight Mach Number of 0.9

A Design Study of Leading-Edge Inlets for Unswept Wings

Pressure Coefficients at Mach Numbers from 0.60 to 0.85 for a Semispan Wing with NACA 0012-64 Section, 20-Percent-Chord Plain Aileron, and 0 Degree and 45 Degree Sweepback

Effect of Retractable Ignition Plug on Plug Fouling by Carbon Deposits

Investigation at a Mach Number of 1.93 to Determine Lift, Drag, Pitching-Moment, and Average Downwash Characteristics for Several Missile Configurations Having Rectangular Wings and Tails of Various Spans

Further Investigation of a Gas Turbine with National Bureau of Standards Body 4811C Ceramic Rotor Blades

Altitude-Chamber Performance of British Roll-Royce Nene II Engine 4: Effect of Operational Variables on Temperature Distribution at Combustion-Chamber Outlets

A Lift-Cancellation Technique in Linearized Supersonic-Wing Theory

On the Theory of the Propagation of Detonation in Gaseous Systems

On the Particular Integrals of the Prandtl-Busemann Iteration Equations for the Flow of a Compressible Fluid

Laws of Flow in Rough Pipes

Experiments to Determine Neighborhood Reactions to Light Airplanes With and Without External Noise Reduction

Isentropic Phase Changes in Dissociating Gases and the Method of Sound Dispersion for the Investigation of Homogeneous Gas Reactions With Very High Speed

Isentropic Phase Changes in Dissociating Gases and the Method of Sound Dispersion for the Investigation of Homogeneous Gas Reactions With Very High Speed

Dependence of the Elastic Strain Coefficient of Copper on the Pre-Treatment

The Development of a Hollow Blade for Exhaust Gas Turbines

General Solution of Prandtl's Boundary-Layer Equation

Formulas for the Supersonic Loading, Lift, and Drag of Flat Swept-Back Wings With Leading Edges Behind the Mach Line

Effect of Intense Sound Waves on a Stationary Gas Flame

Theory of Plane, Symmetrical Intake Diffusers

Turbulence and Heat Stratification

The Solution of the Laminar-Boundary-Layer Equation for the Flat Plate for Velocity and Temperature Fields for Variable Physical Properties and for the Diffusion Field at High Concentration

The Stability of the Compression Cover of Box Beams Stiffened by Posts

Contribution to the Problem of Buckling of Orthotropic Plates, With Special Reference to Plywood

Some Effects of Nonlinear Variation in the Directional-Stability and Damping-in-Yawing Derivatives on the Lateral Stability of an Airplane

Analysis of Turbulent Free-Convection Boundary Layer on Flat Plate

The Diffusion of a Hot Air Jet in Air in Motion Part 2: The Flow Field in the Transition Zone

Graphical Determination of Wall Temperatures for Heat Transfers Through Walls of Arbitrary Shape

Investigation of Downwash, Sidewash, and Mach Number Distribution Behind a Rectangular Wing at a Mach Number of 2.41

Some Features of Artificially Thickened Fully Developed Turbulent Boundary Layers with Zero Pressure Gradient

Small Bending and Stretching of Sandwich-Type Shells

Supersonic Flow Around Circular Cones at Angles of Attack

A General Integral Form of the Boundary-Layer Equation for Incompressible Flow With an Application to the Calculation of the Separation Point of Turbulent Boundary Layers

The External-Shock Drag of Supersonic Inlets Having Subsonic Entrance Flow

Preliminary Investigation of Reflections of Oblique Waves from a Porous Wall

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine: 1: Rotor Blades With 10 Tubes in Cooling-Air Passages

Wind-Tunnel Investigation of a 0.6-Scale Model of Hughes MX-904 Tail Surface at Supersonic Speeds: Tail Attached to a Segment of the Foreshortened Body

Wind-Tunnel Investigation of a 1/6-Scale Model of the Bumblebee XPM Missile at High Subsonic Speeds

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine 2: Rotor Blades With 15 Fins in Cooling-Air Passages

Effect of Nose Shape and Wing Thickness Ratio on the Drag at Zero Lift of a Missile Having Triangular Wings and Tails

Investigation of Power Requirements for Ice Prevention and Cyclical De-Icing of Inlet Guide Vanes with Internal Electric Heaters

Model Ditching Investigations of Three Airplanes Equipped With Hydro-Skis

Photomicrographic Investigation of Spontaneous Freezing Temperatures of Supercooled Water Droplets


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