Search U.S. government technical reports digitized or harvested by TRAIL.
Engine performance with a hydrogenated safety fuel
Simplified aerodynamic analysis of the cyclogiro rotating wing system
Charts for determining the pitching moment of tapered wings with sweepback and twist
The 1933 Contest for the Deutsch De La Meurthe Trophy
A Complete Tank Test of a Model of a Flying-Boat Hull - N.A.C.A. Model No.11
Working Charts for the Determination of Propeller Thrust at Various Air Speeds
Guide Vanes for Deflecting Fluid Currents With Small Loss of Energy
Recent Results of Turbulence Research
Attaining a Steady Air Stream in Wind Tunnels
The high-speed tank of the Hamburg Shipbuilding Company
The Bernard 82 military airplane (French) : a long-range monoplane
Aerodynamic principles of the direct lifting propeller
The Aachen wind-tunnel balance
Experiments with planing surfaces
Analysis of spinning in a monoplane wing by the induction method as compared with the strip method
The behavior under shearing stress of duralumin strip with round, flanged holes
Air conditions close to the ground and the effect on airplane landings
The calculation of take-off run
Experimental investigation of the Robinson-type cup anemometer
Heat transfer from finned metal cylinders in an air stream
The aerodynamic effects of wing cut-outs
Air flow in a separating laminar boundary layer
The estimation of maximum load capacity of seaplanes and flying boats
Static thrust of airplane propellers
Relative loading on biplane wings
Tests of 16 related airfoils at high speed
General Theory of Aerodynamic Instability and the Mechanism of Flutter
Resume of Present Data on Load Distribution on Slots and Flaps, Special Report
Preliminary Wind-Tunnel and Flight Tests of a Balanced Split Flap, Special Report
Wing-Nacelle-Propeller Tests - Comparative Tests of Liquid-Cooled and Air-Cooled Engine Nacelles
The Effect of Spray Strips on the Take-Off Performance of a Model of a Flying-Boat Hull
Potential Flow About Elongated Bodies of Revolution
Scale Effect on Clark Y Airfoil Characteristics From NACA Full-Scale Wind-Tunnel Tests
Some Factors Affecting Combustion in an Internal-Combustion Engine
An Analysis of Longitudinal Stability in Power-Off Flight With Charts for Use in Design
Analysis of 2-Spar Cantilever Wings With Special Reference to Torsion and Load Transference
The Short "Scylla" Commercial Airplane (British): An All-Metal Biplane
The British Klemm "Eagle" Commercial Airplane: A Low-Wing Cantilever Monoplane
The De Havilland "Comet" Long-Range Airplane (British): A Low-Wing Cantilever Monoplane
Avro 642 Commercial Airplane (British): A High-Wing Cantilever Monoplane