Search U.S. government technical reports digitized or harvested by TRAIL.
Thermodynamic Charts for Internal-Combustion-Engine Fluids
Elastic Buckling of Outstanding Flanges Clamped at One Edge and Reinforced by Bulbs at Other Edge
On Internal Damping of Rotating Beams
Office of Naval Research and NACA Metallurgical Investigation of a Large Forged Disc of S-816 Alloy
Flight Investigation in Climb and at High Speed of a Two-Blade and a Three-Blade Propeller
Matrix Methods for Calculating Cantilever-Beam Deflections
Reinforced Circular Cutouts in Plane Sheets
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
Pressure Distributions on Thin Conical Body of Elliptic Cross Section at Mach Number 1.89
Investigation of Performance of Typical Inlet Stage of Multistage Axial-Flow Compressor
An Empirical Method for Estimating Trailing-Edge Loads at Transonic Speeds
Tests of the NACA 64-010 and 64A010 Airfoil Sections at High Subsonic Mach Numbers
Investigation of Fretting by Microscopic Observation
Effect of Reynolds Number in Turbulent-Flow Range on Flame Speeds of Bunsen Burner Flames
Application of Radial-Equilibrium Condition to Axial-Flow Compressor and Turbine Design
Line-Vortex Theory for Calculation of Supersonic Downwash
Equilibrium Operating Performance of Axial-Flow Turbojet Engines by Means of Idealized Analysis
Plastic Buckling of a Rectangular Plate Under Edge Thrusts
On Stability of Free Laminar Boundary Layer Between Parallel Streams
Investigation of Separation of the Turbulent Boundary Layer
Characteristics of Low-Aspect-Ratio Wings at Supercritical Mach Numbers
Calculation of Counterrotating Propellers
Behavior of the Laminar Boundary Layer for Periodically Oscillating Pressure Variation
Compression Shocks in Two-Dimensional Gas Flows
Summary of Information Relating to Gust Loads on Airplanes
Stability and Control Data Obtained from First Flight of X-4 Airplane
On Reflection of Shock Waves from Boundary Layers
Investigation of Aerodynamic and Icing Characteristics of Recessed Fuel-Vent Configurations
Investigation of Icing Characteristics of Typical Light Airplane Engine Induction Systems