Search U.S. government technical reports digitized or harvested by TRAIL.
Tests in the gust tunnel of a model of the XBM-1 airplane
A comparison of several tapered wings designed to avoid tip stalling
A flight investigation of the distribution of ice-inhibiting fluids on a propeller blade
Local instability of columns with I-, Z-, channel, and rectangular-tube sections
A preliminary study of the prevention of ice on aircraft by the use of engine-exhaust heat
Experiments on the Recovery of Waste Heat in Cooling Ducts, Special Report
Preliminary Model Tests of a Wing-Duct Cooling System for Radial Engines, Special Report
Two-Stroke-Cycle Engines With Unsymmetrical Control Diagram (Supercharged Engines)
Radiator Design and Installation
Pressure Distribution on the Fuselage of a Midwing Airplane Model at High Speeds
Profile-Drag Investigation of an Airplane Wing Equipped with Rubber Inflatable De-Icer
[Memorandums on the Subject of Propellers]
Tests of Several Model Nacelle-Propeller Arrangements in Front of a Wing
Tests of Airfoils Designed to Delay the Compressibility Burble
Correlation of Cooling Data From an Air-Cooled Cylinder and Several Multicylinder Engines
Tests of NACA 0009, 0012, and 0018 Airfoils in the Full-Scale Tunnel
Experimental Investigation of the Momentum Method for Determining Profile Drag
Mechanical Properties of Flush-Riveted Joints
Experimental and Analytical Investigation of a Monocoque Wing Model Loaded in Bending
The Way to Increased Airplane Engine Power
The Power of Aircraft Engines at Altitude
The Limit of Stability of a Curved Plate Strip Under Shear and Axial Stresses
Investigation of the Lift Distribution Over the Separate Wings of a Biplane
Dynamic Stability of a Helicopter With Hinged Rotor Blades
Effects of Propellers and of Vibration on the Extent of Laminar Flow on the NACA 27-212 Airfoil
The Hydrodynamic Theory of Detonation
The Enlarged N.A.C.A. Tank, and Some of Its Work
The Effect of Streamlining the Aterbody of an N.A.C.A. Cowling
Engine Knock and Combustion Chamber Form
Forces and Moments on a Yawed Airfoil
Contribution to the Aerodynamics of Rotating-Wing Aircraft
Theory of Two-Dimensional Potential Flow About Arbitrary Wing Sections
The Theory of Contra-Vanes Applied to the Propeller
Theoretical and Experimental Study of Ignition Lag and Engine Knock
Stability of Rectangular Plates With Longitudinal or Transverse Stiffeners Under Uniform Compression
Contribution to the Theory of the Heated Duct Radiator
Knocking in the Otto-Cycle Engine
Meteorological-Physical Limitations of Icing in the Atmosphere
The Effect of the Masses of the Controls on the Longitudinal Stability With Free Elevator Part 1