Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
1349 results returnedSearch results
- Spinning Characteristics of Wings 3: A Rectangular and Tapered Clark Y Monoplane Wing with Rounded Tips
- Pressure drop across finned cylinders enclosed in a jacket
- Flight tests of an airplane showing dependence of the maximum lift coefficient on the test conditions
- Notes on Factors Affecting Geometrical Arrangement of Tricycle-Type Landing Gears
- Tandem Air Propellers
- Synthetic Resins in Aircraft Construction - Their Composition, Properties, Present State of Development and Application to Light Structures
- The Transition Phase in the Take-Off of an Airplane, Special Report
- A Study of Transparent Plastics for use on Aircraft, Special Report
- Supplement to A Study of Transparent Plastics for use on Aircraft
- Stability of Castering Wheels for Aircraft Landing Gears, Special Report
- Tests in the Variable-Density Tunnel of Seven Tapered Wings Having N.A.C.A. 230 Mean Lines, Special Report
- Energy Loss, Velocity Distribution, and Temperature Distribution for a Baffled Cylinder Model, Special Report
- Accelerations in Landing with a Tricycle-Type Landing Gear
- The Ground Effect on Lifting Propellers
- Some Experiments on the Slipstream Effect
- The Design of Airplane-Engine Superchargers
- Annual Report of the National Advisory Committee for Aeronautics (22nd). Administrative Report Including Technical Report Nos. 542 to 576
- Aerodynamic Characteristics of NACA 23012 and 23021 Airfoils With 20-Percent-Chord External-Airfoil Flaps of NACA 23012 Section
- An Analytical and Experimental Study of the Effect of Periodic Blade Twist on the Thrust, Torque, and Flapping Motion of an Autogiro Rotor
- Measurements of Intensity and Scale of Wind-Tunnel Turbulence and Their Relation to the Critical Reynolds Number of Spheres
- Full-Scale Tests of a New Type NACA Nose-Slot Cowling
- General Airplane Performance
- Resume and analysis of NACA lateral control research
- Spinning characteristics of the XN2Y-1 airplane obtained from the spinning balance and compared with results from the spinning tunnel and from flight tests
- Pressure distribution over a rectangular airfoil with a partial-span split flap
- The experimental and calculated characteristics of 22 tapered wings
- The variation with Reynolds number of pressure distribution over an airfoil section
- Wind-tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps
- A study of flying-boat take-off
- Hydrodynamic and aerodynamic tests of models of flying-boat hulls designed flow aerodynamic drag - NACA models 74, 74-A, and 75
- The increase in frictional resistance caused by various types of rivet heads as determined by tests of planing surfaces
- Tank Tests to Show the Effect Rivet Heads on the Water Performance of a Seaplane-Float
- Some aspects of the stalling of modern low-lying monoplanes
- A new spinning-test method
- The design of floats
- Behavior of a plate strip under shear and compressive stresses beyond the buckling limit
- Behavior of static pressure heads at high speeds
- Effect of propeller slipstream on wing and tail
- Systematic airfoil tests in the large wind tunnel of the DVL
- The Focke helicopter
- Application and testing of transparent plastics used in airplane construction
- The Dornier wind tunnel
- A flight comparison of conventional ailerons on a rectangular wing and of conventional and floating wing-tip ailerons on a tapered wing
- Heat transfer to fuel sprays injected into heated gases
- Aerodynamic characteristics of a large number of airfoils tested in the variable-density wind tunnel
- Air flow in the boundary layer of an elliptic cylinder
- Comparative flight and full-scale wind-tunnel measurements of the maximum lift of an airplane
- The aerodynamic characteristics of four full-scale propellers having different plan forms
- Airfoil section characteristics as applied to the prediction of air forces and their distribution on wings
- Interrelation of exhaust-gas constituents