Search U.S. government technical reports digitized or harvested by TRAIL.
Heinkel He 64 C sport airplane (German) : a two-seat low-wing cantilever monoplane
A complete tank test of a model of a flying-boat hull - N.A.C.A. Model No. 11
Present Status of Lateral-Control Devices for Use With Split Flaps, Special Report
Development of Air-Cooled Engines With Blower Cooling
The Flight of an Autogiro at High Speed
Strength Tests of Thin-Walled Duralumin Cylinders in Compression
Wing-Fuselage Interference, Tail Buffeting, and Air Flow About the Tail of a Low-Wing Monoplane
Aircraft Power-Plant Instruments
The Westland "Wallace" General-Purpose Airplane (British): An All-Metal Biplane
The Shackleton-Murray SM-1 Light Airplane: A Two-Place High-Wing Monoplane
The D.H. 85 "Leopard Moth" Airplane (British): A Three-Seat Cabin High-Wing Monoplane
The d.h."Dragon Moth" Commercial Airplane (British): A Twin-Engine 6-Passenger Biplane
The Dewoitine D.332 Commercial Airplane (French): A Three-Engine All-Metal Low-Wing Monoplane
The Dewoitine D.500 Pursuit Airplane (French): An All-Metal Cantilever Low-Wing Monoplane
The Comper "Mouse" Commercial Airplane (British): A Three-Seat Cabin Low-Wing Monoplane
Experiments With Needle Bearings
Flight-Test Data on the Static Fore-and-Aft Stability of Various German Airplanes
The D.V.L. Gliding-Angle Control (W. Hübner Design)
Increasing the Volumetric Efficiency of Diesel Engines by Intake Pipes
Determination of Inherent Stresses by Measuring Deformations of Drilled Holes
The Critical Shear Load of Rectangular Plates
Practical Experiences With Lightning Discharges to Airplanes
Trend of Airplane Flight Characteristics
The Theory of the Strandgren Cyclogyro
Pressure Rise, Gas Vibrations and Combustion Noises During the Explosion of Fuels
Knowledge Gained From Practical Experience in the Designing of Aircraft Engines
Dynamic Breaking Tests of Airplane Parts
Dimensions of Twin Seaplane Floats
The N.A.C.A. Tank: A High-Speed Towing Basin for Testing Models of Seaplane Floats
The N.A.C.A. High-Speed Wind Tunnel and Tests of Six Propeller Sections
Interference on an Airfoil of Finite Span in an Open Wind Tunnel
The Process of Separation in the Turbulent Friction Layer
Experimental Verification of the Theory of Wind-Tunnel Boundary Interference
Tests for the Elimination of Tail Flutter
A Simple Method for Increasing the Lift of Airplane Wings by Means of Flaps
Pressure and Frictional Resistance of a Cylinder at Reynolds Numbers 5,000 to 40,000
The Problem of the Propeller in Yaw With Special Reference to Airplane Stability
Results of Extended Tests of the Focke-Wulf F 19a "Ente," a Tail-First Airplane