Search U.S. government technical reports digitized or harvested by TRAIL.
Heat Transfer in Geometrically Similar Cylinders
Formulas for Use in Boundary-Layer Calculations on Low-Drag Wings
Internally Finned Honeycomb Radiators
Aluminum-Zinc-Magnesium-Copper Casting Alloys
Performance Characteristics of an Aircraft Engine with Exhaust Turbine Supercharger, Special Report
Temperature Recording in High-Speed Gases
High-speed wind-tunnel tests of the NACA 23012 and 23012-64 airfoils
Restraint provided a flat rectangular plate by a sturdy stiffener along an edge of the plate
The Selection of Propellers for High Thrust at Low Airspeed
A semi-rational criterion for unsymmetrical gust loads
Shear lag in box beams methods of analysis and experimental investigations
The effect of external shape upon the drag of a scoop
Drag Measurements of a Protruding 0.50-Caliber Machine Gun
Dynamic stress calculations for two airplanes in various gusts
Determination of optimum plan forms for control surfaces
Test of single-stage axial-flow fan
Investigation of naphthalene as a possible aircraft fuel
Wind-Tunnel Tests of Eight-Blade Single and Dual-Rotating Propellers in the Tractor Position
Wind-Tunnel Tests of Four Curtiss Propellers Embodying Different Blade Sections
Pressure distribution over an airfoil with a balanced split flap
Pressure distribution over an NACA 23012 airfoil with a fixed slot and a slotted flap
Power-off wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane
Wind-tunnel investigation of 20-percent-chord plain and Frise ailerons on an NACA 23012 airfoil
Wind-tunnel investigation of a section of the horizontal tail surface for the Bell XP-63 airplane
Nonstationary flow about a wing-aileron-tab combination including aerodynamic balance
Notes on the Stability and Control of Tailless Airplanes
Internal-Flow Systems for Aircraft
Flutter calculations in three degrees of freedom
Determination of control-surface characteristics from NACA plain-flap and tab data
Correction of the Lifting-Line Theory for the Effect of the Chord
The Calculation of Span Load Distributions of Swept-Back Wings
Methods of Analyzing Wind-Tunnel Data for Dynamic Flight Conditions