Search U.S. government technical reports digitized or harvested by TRAIL.
Some Elementary Principles of Shell Stress Analysis With Notes on the Use of the Shear Center
Some fundamental considerations in regard to the use of power in landing an airplane
The Effects of Some Surface Irregularities on Wing Drag
Torsional stability of aluminum alloy seamless tubing
Wind-Tunnel Investigation of Ground Effect on Wings With Flaps
Compression-ignition engine performance with undoped and doped fuel oils and alcohol mixtures
A simplified method for the calculation of airfoil pressure distribution
An Experimental Investigation of the Normal Acceleration of an Airplane Model in a Gust
An investigation of the drag of windshields in the 8-foot high-speed wind tunnel
Static Thrust and Power Characteristics of Six Full-Scale Propellers
Calculation of the Aerodynamic Characteristics of Tapered Wings With Partial-Span Flaps
Experimental Verification of the Theory of Oscillating Airfoils
An Electrical-Type Indicating Fuel Flowmeter
Engine Operation in Flight for Minimum Fuel Consumption
The Effect of Streamlining the Afterbody of an N.A.C.A. Cowling
Design of Centrifugal Impeller Blades
Acceleration, Stress, and Deflection Measurements on the XB-15 Bomber in Gusty Air
Investigation of an Electrically Heated Airplane Windshield for Ice Prevention, Special Report
An Investigation of the Prevention of Ice on the Airplane Windshield
An Investigation of the Drag of Windshields in the 8-Foot High-Speed Wind Tunnel
High-Speed Tests of Radial-Engine Cowlings
Intercooler Design for Aircraft, Special Report
Ground-cooling and flight tests of an airplane equipped with a nose-blower engine cowling
High-Speed Tests of Conventional Radial-Engine Cowlings
Tests of Several Model Nacelle-Propeller Arrangements in Front of a Wing
Estimation of critical speeds of airfoils and streamline bodies
The problem of cooling an air-cooled cylinder on an aircraft engine
Longitudinal stability and control with special reference to slipstream effects
Heat-transfer tests of a steel cylinder barrel with aluminum fins of optimum proportions
Drag analysis of single-engine military airplanes tested in the NACA full-scale wind tunnel
The design of cooling ducts with special reference to the boundary layer at the inlet