Search U.S. government technical reports digitized or harvested by TRAIL.
Cooling and Performance Tests of a Continental A-75 Engine
Variation of Properties Throughout Cross Section of Two Extruded Shapes
Tests of Bell XP-63 Low-Drag Wing Model With Split Flap
The Oscillating Wing With Aerodynamically Balanced Elevator
On the Use of Residue Theory for Treating the Subsonic Flow of a Compressible Fluid
Researches on Direct Injection in Internal-Combustion Engines
Static Characteristics of Curtiss Propellers Having Different Blade Sections
Experimental Investigations on Freely Exposed Ducted Radiators
Dynamic Similitude in Internal-Combustion Engines
A Flight Investigation of Internally Balanced Sealed Ailerons
Comparison of Automatic Control Systems
The Creep of Laminated Synthetic Resin Plastics
The Elliptic Wing Based on the Potential Theory
The Reaction Jet as a Means of Propulsion at High Speeds
Stress Analysis of Circular Frames
Use of Charts for Flow Discharge Calculations
Inertia of Dynamic Pressure Arrays
Square Plate With Clamped Edges Under Normal Pressure Producing Large Deflections
Stagnation Temperature Recording
Contribution to the Aerodynamics of Rotating-Wing Aircraft: Part 2
Requirements for Satisfactory Flying Qualities of Airplanes
On the Calculation of Flow Past an Infinite Screen of Thin Airfoils
Factors Influencing the Fatigue Strength of Materials
The Efficiency of Combustion Turbines With Constant-Pressure Combustion
Effect of Aging on Mechanical Properties of Aluminum-Alloy Rivets
Wind-Tunnel Investigation of an NACA 23021 Airfoil With Two Sizes of Balanced Split Flaps
Boundary Layer Removal by Suction
Requirements for Satisfactory Flying Qualities of Airplanes
Development of Cowling for Long-Nose Air-Cooled Engine in the NACA Full-Scale Wind Tunnel
Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel
The Compressive Yield Strength of Extruded Shapes of 24ST Aluminum Alloy
Supplement to Comparison of Automatic Control Systems
Spin Tests of Two Models of a Low-Wing Monoplane to Investigate Scale Effect in the Model Test Range