Search U.S. government technical reports digitized or harvested by TRAIL.
The Lift Distribution of Wings With End Plates
On the Determination of the Take-Off Characteristics of a Seaplane
Performance of Rotating-Wing Aircraft
Model Experiments on the Forces and Moments Acting on an End Plate Fitted to a Wing
The Effect of Continuous Weathering on Light Metal Alloys Used in Aircraft
Heat-Transfer Processes in Air-Cooled Engine Cylinders
Two-Dimensional Subsonic Compressible Flow Past Elliptic Cylinders
The Column Strength of Two Extruded Aluminum-Alloy H-Sections
Longitudinal Stability in Relation to the Use of an Automatic Pilot
Preliminary Fatigue Studies on Aluminum Alloy Aircraft Engines
Tests of N-85, N-86 and N-87 Airfoil Sections in the 11-Inch High Speed Wind Tunnel
Generalized Analysis of Experimental Observations in Problems of Elastic Stability
Fatigue Testing of Wing Beam by the Resonance Method
Wind-Tunnel Tests of a Clark Y Wing Having Split Flaps With Gaps
Wind-Tunnel Tests of Carburetor-Intake Rams
Fuel Consumption of a Carburetor Engine at Various Speeds and Torques
Theoretical Study of Various Airplane Motions After Initial Disturbance
The Present Status of Airship Construction, Especially of Airship-Framing Construction
Load Tests on a Stiffened Circular Cylindrical Shell
Theoretical stability and control characteristics of wings with various amounts of taper and twist
Tests in the variable-density wind tunnel of the NACA 23012 airfoil with plain and split flaps
Mechanism of flutter: A theoretical and experimental investigation of the flutter problem
A study of the torque equilibrium of an autogiro rotor
Pressure distribution over an NACA 23012 airfoil with a slotted and a plain flap
A study of air flow in an engine cylinder
Wind-Tunnel Investigation of an NACA 23012 Airfoil with Various Arrangements of Slotted Flaps
On some reciprocal relations in the theory of nonstationary flows
The Aerodynamic Drag of Five Models of Side Floats N.A.C.A. Models 51-E, 51-F, 51-G, 51-H, 51-J
N.A.C.A. Stall-Warning Indicator
Noise From Propellers With Symmetrical Sections at Zero Blade Angle, 2
Tests of a Contra-Propeller for Aircraft
Scavenging a Piston-Ported Two-Stroke Cylinder
Discharge Characteristics of a Simulated Unit Injection System
The Pressure Available for Ground Cooling in Front of the Cowling of Air-Cooled Airplane Engines
A method of rapidly estimating the position of the laminar separation point