Search U.S. government technical reports digitized or harvested by TRAIL.
Tables of Stiffness and Carry-Over Factor for Structural Members Under Axial Load
Tank Tests of Model 36 Flying Boat Hull
The N.A.C.A. Optical Engine Indicator
Gyroscopic Instruments for Instrument Flying
The drag of inflatable rubber de-icers
The effect of air-passage length on the optimum fin spacing for maximum cooling
Effect of spark-timing regularity on the knock of engine performance
Tank tests of a model of one hull of the Savoia S-55-X flying boat - N.A.C.A. Model 46
The estimation of the rate of change of yawing moment with sideslip
Flight and wind-tunnel tests of an XBM-1 dive bomber
Spinning characteristics of wings 5: N.A.C.A. 0009, 23018, and 6718 monoplane wings
Principles involved in the cooling of a finned and baffled cylinder
Operational treatment of the nonuniform-lift theory in airplane dynamics
Preliminary Full-Scale Wind-Tunnel Investigation of Wing Ducts for Radiators, Special Report
Static Longitudinal Stability and Longitudinal Control of Autogiro Rotors
Wind-Tunnel Investigation of Air Inlet and Outlet Openings for Aircraft, Special Report
The Effect of Surface Irregularities on Wing Drag 1 - Rivets and Spot Welds
The Effect of Surface Irregularities on Wing Drag 2 - Lap Joints
The Effect of Surface Irregularities on Wing Drag 4 - Manufacturing Irregularities
The Effect of Surface Irregularities on Wing Drag 3 - Roughness
The Conversion of Energy in a Radiator
Full-Scale Wind-Tunnel Investigation of Wing Cooling Ducts, Special Report
On the Theory of Hydrofoils and Planing Surfaces
Comparison of free-spinning wind-tunnel results with corresponding full-scale spin results
Investigation in the 7-by-10 Foot Wind Tunnel of Ducts for Cooling Radiators within an Airplane Wing
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