Browse TRAIL Inventories

Quantitative Study of Variations in Concentration of Glycerol and Aerosol OT on Foaming Volume of Oil at Room Temperature

Direct-Reading Design Charts for 24S-T Aluminum-Alloy Flat Compression Panels Having Longitudinal Formed Z-Section Stiffeners

Summary of the Availability and Performance Problems of High Octane Number Fuels

Preliminary Investigation of 3-Inch Slotted Transonic Wind-Tunnel Test Sections

Spin-Tunnel Investigation of the Jettisoning of External Fuel Tanks in Spins

Bibliography of Classified Aircraft-Fire Literature

Study by NACA Wing-Flow Method of Transonic Drag Characteristics of a Blunt-Nose Body of Revolution and Comparison with Results for a Sharp-Nose Body

Pressure Distributions on Thin Conical Body of Elliptic Cross Section at Mach Number 1.89

Preliminary Aerodynamic Investigation of the Effect of Camber on a 60 Degree Delta Wing with Round and Beveled Leading Edges

Investigation of Performance of Typical Inlet Stage of Multistage Axial-Flow Compressor

Lateral-Control Investigation on a 37 Degree Sweptback Wing of Aspect Ratio 6 at a Reynolds Number of 6,800,000

An Empirical Method for Estimating Trailing-Edge Loads at Transonic Speeds

The Static-Pressure Error of Wing and Fuselage Airspeed Installations of the X-1 Airplanes in Transonic Flight

Tests of the NACA 64-010 and 64A010 Airfoil Sections at High Subsonic Mach Numbers

Investigation of Fretting by Microscopic Observation

Investigations on the Stability, Oscillation, and Stress Conditions of Airplanes With Tab Control: Second Partial Report: Application of the Solutions Obtained in the First Partial Report to Tab-Controlled Airplanes

Initial Experiments on Flutter of Unswept Cantilever Wings at Mach Number 1.3

High-Speed Wind-Tunnel Investigation of a Sweptback Wing With an Added Triangular Area at the Center

General Theory of Aerodynamic Instability and the Mechanism of Flutter

Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)

Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6)

Aerodynamic Properties of Cruciform-Wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds

A Statistical Study of Wave Conditions at Four Open-Sea Localities in the North Pacific Ocean

Ambient Pressure Determination at High Altitudes by Use of Free-Molecule Theory

Wind-tunnel investigation of the spinning characteristics of a model of a twin-tail low-wing personal-owner-type airplane with linked and unlinked rudder and aileron controls

Critical Stress of Ring-Stiffened Cylinders in Torsion

Vibration Survey of Blades in 10-Stage Axial-Flow Compressor 1: Static Investigation

Flow Measurement by Means of Light Interference

Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the Grumman XF9F-2 Airplane with Wing-Tip Tanks Installed

Gas Motion in a Local Supersonic Region and Conditions of Potential-Flow Breakdown

Heat Transmission in the Boundary Layer

Jet Diffusion in Proximity of a Wall

Lift Force of an Arrow-Shaped Wing

Annual Report of the National Advisory Committee for Aeronautics (32nd). Administative Report Including Technical Report Nos. 834 to 862

Annual Report of the National Advisory Committee for Aeronautics (30th). Administrative Report Including Technical Report Nos. 774 to 803

Annual Report of the National Advisory Committee for Aeronautics (31st). Administrative Report Including Technical Report Nos. 804 to 833

The Effects of Horizontal-Tail Location and Wing Modifications on the High-Speed Stability and Control Characteristics of a 01.17-Scale Model of the McDonnell XF2H-1 Airplane (TED No, NACA DE336)

Report on Investigation of Developed Turbulence

Performance of Single-Stage Turbine of Mark 25 Torpedo Power Plant with Two Special Nozzles 1 - Efficiency with 0.45-inch Rotor Blades

Preliminary Analysis of Axial-Flow Compressors Having Supersonic Velocity at the Entrance of the Stator

General Characteristics of a Airspeed System using Fuselage Static Vents on a Swept-Wing Airplane

Free-Spinning-Tunnel Investigation of a 1/20-Scale Model of the McDonnell XF2H-1 Airplane

Performance of Axial-Flow Supersonic Compressor of XJ55-FF-1 Turbojet Engine 2 - Performance of Inlet Guide Vanes as Separate Component

Comparison of Water-Load Distributions Obtained during Seaplane Landings with Bureau of Aeronautics Specifications. TED No. NACA 2413

The Compressible Flow Past Various Plane Profiles Near Sonic Velocity

Computation of Thin-Walled Prismatic Shells

Constant-Pressure Combustion Charts Including Effects of Diluent Addition

Contribution to the Problem of Flow at High Speed

Altitude Performance of AN-F-58 Fuels in British Rolls-Royce Nene Single Combustor

Altitude-Test-Chamber Investigation of McDonnell Afterburner on J34 Engine


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