Browse TRAIL Inventories

Tests of the landing on water of a model of a high-speed airplane - Langley tank model 229

Comparison of the transonic drag characteristics of two wing-body combinations differing only in the location of the 45 degree sweptback wing

Calculations of the Supersonic Wave Drag of Nonlifting Wings with Arbitrary Sweepback and Aspect Ratio: Wings Swept Behind the Mach Lines

Lateral stability and control characteristics of an airplane model having 42.8 degree sweptback circular-arc wing with aspect ratio 4.00, taper ratio 0.50, and sweptback tail surfaces

Canopy loads investigation for the F6F-3 airplane

Investigation of Pressure Distribution over an Extended Leading-Edge Flap on a 42 Degrees Sweptback Wing

Pressure-distribution measurements on a full-scale horizontal tail surface for a Mach number range of 0.20 to 0.70

A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot

Measurements of the effects of thickness ratio and aspect ratio on the drag of rectangular-plan-form airfoils at transonic speeds

Preliminary investigation of spoiler lateral control on a 42 degree sweptback wing at transonic speeds

Wind-tunnel development of optimum double-slotted-flap configurations for seven thin NACA airfoil sections

Observations on an aileron-flutter instability encountered on a 45 degree swept-back wing in transonic and supersonic flight

Preliminary Tests to Determine the Maximum Lift of Wings at Supersonic Speeds

Wind-Tunnel Investigation of Bomb-Bay Configurations Intended to Minimize the Tumbling of Light-Weight Bombs

Six-Component Measurements on a Straight and a 35 Degree Swept-Back Trapezoidal Wing With and Without Split Flaps

Practical Possibilities of High-Altitude Flight with Exhaust-Gas Turbines in Connection with Spark Ignition Engines Comparative Thermodynamic and Flight Mechanical Investigations

Performance Charts for a Turbojet System

Performance of a Mixed-Flow Impeller in Combination with Semivaneless Diffuser

Some Tests and Calculations Pertaining to the Dive Path and to Wing and Tail Loads in the Accident to Eastern Airlines C54B Airplane, NC-88814, Near Bainbridge, Maryland, May 30, 1947

Stability of Plates and Shells Beyond the Proportional Limit

The Separation of Flow Due to Compressibility Shock

Simulated Altitude Investigation of Stewart-Warner Model 906-B Combustion Heater

Systematic Wind-Tunnel Measurements on Missiles

The Calculation of Compressible Flows with Local Regions of Supersonic Velocity

A Time History of Control Operation of a C-54 Airplane in Blind Landing Approaches

Results of Flight Test of an Automatically Stabilized Model C (Swept Back) Four-Wing Tiamat

Supersonic Wave Drag of Sweptback Tapered Wings at Zero Lift

Scale Effect and Optimum Relations for Sea Surface Planning

Theoretical Evaluation of Methods of Cooling the Blades of Gas Turbines

Vibration Survey of Blades in 19XB Axial-Flow Compressor 2: Dynamic Investigation

An Analysis of the Full-Floating Journal Bearing

Wind-Tunnel Tests of a 1/8-Scale Powered Model of the XTB3F-1 Airplane, TED No. NACA 2382

A Theory of Unstaggered Airfoil Cascades in Compressible Flow

A Theory of Unstaggered Airfoil Cascades in Compressible Flow

Tests of a Horizontal-Tail Model through the Transonic Speed Range by the NACA Wing-Flow Method

Pressure-Distribution Measurements on Unyawed Swept-Back Wings

Tests of Cascades of Airfoils for Retarded Flow

Russian Laminar Flow Airfoils 3rd Part: Measurements on the Profile No. 2315 BIS with Ava-Nose Flap

Some Aerodynamic Relations for an Airfoil in Oblique Flow

Temperatures and Stresses on Hollow Blades For Gas Turbines

Test Report on Measurements on a Series of Tapered Wings of Small Aspect Ratio (Trapezoidal Wing with Fuselage)

Infinitesimal Conical Supersonic Flow

On Combustion in a Turbulent Flow

On the Vortex Sound from Rotating Rods

On the Application of the Energy Method to Stability Problems

On the Theory of the Unsteady Motion of an Airfoil

Preliminary Report on the Fundamentals of the Control of Turbine-Propeller Jet Power Plant

Investigation of the Operating Properties of the Leakage Current Anemometer

The Effect of Turbulence on the Flame Velocity in Gas Mixtures

Equations for Adiabatic but Rotational Steady Gas Flows Without Friction


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