Search U.S. government technical reports digitized or harvested by TRAIL.
Simple Curves for Determining the Effects of Compressibility on Pressure Drop Through Radiators
High-Altitude Cooling 3: Radiators
Wind-Tunnel Investigation of Ailerons on a Low-Drag Airfoil 3: The Effect of Tabs
The Effect of Engine Conditions on the Lead Susceptibility of Paraffinic Fuels
Tests of NACA 65(216)-420 and 66(218)-420 Airfoils at High Speeds
Cylinder-Head Cooling by Means of a Shield in the Exhaust Passage
Air-Consumption Parameters for Automatic Mixture Control of Aircraft Engines
Determination of the Stresses Produced by the Landing Impact in the Bulkheads of a Seaplane Bottom
Comparative Results of Tests on Several Different Types of Nozzles
Compressibility Effects on Heat Transfer and Pressure Drop in Smooth Cylindrical Tubes
Determination of the Actual Contact Surface of a Brush Contact
Simply Supported Long Rectangular Plate Under Combined Axial Load and Normal Pressure
On the General Theory of Thin Airfoils for Nonuniform Motion
The "Limiting Line" in Mixed Subsonic and Supersonic Flow of Compressible Fluids
Dynamics of the Inlet System of a Four-Stroke Engine
Investigation of the Behavior of Parallel Two-Dimensional Air Jets
Simplified Truss Stability Criteria
Torsion Test to Failure of a Monocoque Box
Tests of Airfoils Designed to Delay the Compressibility Burble
The Effect of Temperature on Sheet Metals for Airplane Firewalls
Plastic Mountings for Aircraft Windshields
Axial Fatigue of 10 Airplane Wing-Beam Specimens by the Resonance Method
Normal Pressure Tests on Unstiffened Flat Plates
An Interim Report on the Stability and Control of Tailless Airplanes
Protection of Nonmetallic Aircraft From Lightning 3: Electrical Effects in Glider Towlines
Design of power-plant installations pressure-loss characteristics of duct components
Tests of a Thermal Ice-Prevention System for a Wing Leading-Edge Landing-Light Installation
Application of Spring Tabs to Elevator Controls
NACA Investigation of a Jet-Propulsion System Applicable to Flight
On the plane potential flow past a symmetrical lattice of arbitrary airfoils
Analysis of Circular Shell-Supported Frames
Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons
Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers