TRAIL - Technical Report Archive and Image Library

Supplementary Wind-Tunnel Investigation of the Stability of the Jettisonable Nose Section of the X-2 Airplane

Pressure-Distribution Measurements on the Tail Surfaces of a Rotating Model of the Design BFW - M31

Some Effects of Stator Cone Angle and Blade-Tip Leakage on 40 Percent Reaction Turbine Having Rotor-Blade Caps

An Analysis of Supersonic Aerodynamic Heating With Continuous Fluid Injection

Frequency Response of Linear Systems From Transient Data

Take-Off Stability Characteristics of a 1/13-Scale Model of the Consolidated Vultee Skate 7 Seaplane (TED No. NACA DE 338)

The theory of plasticity in the case of simple loading accompanied by strain-hardening

Susceptibility to Welding Cracking, Welding Sensitivity, Susceptibility to Welding Seam Cracking, and Test Methods for These Failures

Systematic Investigations of the Effects of Plan Form and Gap between the Fixed Surface and Control Surface on Simple Flapped Wings

The Influence of the Application of Power during Spin Recovery of Multiengine Airplanes

Investigation of Conditions of Titanium Carbonization - 4

On Wind Tunnel Tests and Computations Concerning the Problem of Shrouded Propellers

On the Theory of the Laval Nozzle

Exact Calculation of Laminar Boundary Layer in Longitudinal Flow Over a Flat Plate With Homogeneous Suction

Experimental Flights for Testing of a Reactor as an Expedient for the Termination of Dangerous Spins

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

Computation of Thin-Walled Prismatic Shells

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

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

Full-Scale Hydrodynamic Evaluation of a Modified Navy J4F-2 Amphibian with a 0.425-Scale XP5M-1 Hull Bottom: TED No. NACA DE325

High Speed Stability and Control Characteristics of a 0.17-Scale Model of the McDonnell XF2H-1 Airplane (TED No. NACA DE 318)

Hydrodynamic Qualities of a 1/10-Size Powered Dynamic Model of the XP5Y-1 Flying Boat in Smooth Water: Langley Tank Model 246, TED No. NACA DE 320

Longitudinal Characteristics of a Semispan Model of the Grumman Airplane Design 83 having a Sweptback Wing and of the Model with a Straight Wing as Determined from Wing-Flow Tests at Transonic Speeds, TED No. NACA DE337

Investigations on the Stability, Oscillation, and Stress Conditions of Airplanes with Tab Control: First Partial Report. Derivation of the Equations of Motion and their General Solutions

Measurement of Oil-Film Pressures in Journal Bearings under Constant and Variable Loads

Performance of Single-Stage Turbine of Mark 25 Torpedo Power Plant with Two Special Nozzles 3: Efficiency with Standard Rotor Blades

On the Motions of an Oscillating System Under the Influence of Flip-Flop Controls

On the Installation of Jet Engine Nacelles on a Wing Fourth Partial Report: Pressure-Distribution Measurements on a Sweptback Wing with Jet Engine Nacelle

Two-Dimensional Compressible Flow in Turbomachines With Conic Flow Surfaces

Two-Dimensional Wing Theory in the Supersonic Range

Two-Dimensional Motion of a Gas at Large Supersonic Velocities

Keyword Search

Published Year

Subject

Author