Browse TRAIL Inventories

Aerodynamic Characteristics and Flap Loads of the Brake-Flap Installation on the 0.40-Scale Model of the F4F-3 Left Wing Panel

Adjustment of Stick Force by a Nonlinear Aileron-Stick Linkage

Aerodynamic Characteristics for Internal-Balance and Frise Type Ailerons on an NACA 6 Series Low-Drag Tip Section of the Wing for the XP-63 Airplane

The Aerodynamic Tests of Three Edo Floats for the SB2U-3, 0S2U-2, and XSB2C-2 Seaplanes - NACA Models 106-K, 107-K, and 125-AH

Aerodynamic Tests of an M-31 Bomb in the 8-Foot High-Speed Tunnel

Self-Ignition and Combustion of Gases

High-Speed Tests of a Model Twin-Engine Low-Wing Transport Airplane

High-Speed Wind-Tunnel Tests of Gun Openings in the Nose of the Fuselage of a 1/4-Scale Model

Flight Measurements of the Aileron Characteristics of a Grumman F4F-3 Airplane

Generalized equations for selection charts for heat exchangers in aircraft

Generalized selection charts for bombers powered by one, two, four, and six 3000-horsepower engines 1: capacity and economy

Generalized selection charts for bombers with four 2000-horsepower engines

High-Speed Tests of a Ducted Body with Various Air-Outlet Openings

Generalized selection charts for bombers powered by two, four, and six 3000-horsepower engines

Shear-lag tests of two box beams with flat covers loaded to destruction

Propeller Blade Stresses Caused by Periodic Displacement of the Propeller Shaft

Correlation of Data on the Statistical Theory of Turbulence

Free-spinning-tunnel tests of a 1/23.75-scale model of the Douglas DC-3 airplane

Effect of airplane design efficiency and engine economy on range

Flight tests of NACA jet-propulsion exhaust stacks on the supermarine spitfire airplane

Full-scale wind-tunnel and flight tests of a Fairchild XR2K-1 airplane with a zap flap and upper-surface aileron-wing installation

The effect of dead rise upon the low-angle type of porpoising

Effect of spring and gravity moments in the control system on the longitudinal stability of the Brewster XSBA-1 airplane

Derivation of charts for determining the horizontal tail load variation with any elevator motion

Tire friction coefficients and their relation to ground-run distance in landing

Summary of V-G records taken on transport airplanes from 1932 to 1942

Tests in the 19-foot pressure tunnel of a 1/2.75-scale model of the F4U-1 airplane with several balanced elevators, full-span flaps, and droppable gas tank

A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls

Tests of four models representing intermediate sections of the XB-33 airplane including sections with slotted flap and ailerons

Calculation of tab characteristics for flight conditions from wind-tunnel data

Characteristics of plain and balanced elevators on a typical pursuit fuselage at attitudes simulating normal-flight and spin conditions

The Characteristics of Two Model Six-Blade Counterrotating Pusher Propellers of Conventional and Improved Aerodynamic Design

Calculated effects of full-span slotted and Fowler flaps on longitudinal stability and control characteristics for a typical fighter-type airplane with various tail modifications

Calibrations of pitot-static tubes at high speeds

Characteristics of beveled-trailing-edge elevators on a typical pursuit fuselage at altitudes simulating-normal flight and spin conditions

Comparison of tightness of 78 degrees machine-countersunk rivets driven in holes prepared with 78 degrees and 82 degrees countersinking tools

Condensation trails: Where they occur and what can be done about them

The longitudinal stability of flying boats as determined by tests of models in the NACA tank 1: methods used for the investigation of longitudinal stability characteristics

Effect of inlet-air velocity distribution on the metering pressure of an injection-type aircraft carburetor

Exhaust-stack nozzle area and shape for individual cylinder exhaust-gas jet-propulsion system

Wind-tunnel tests of single- and dual-rotating tractor propellers of large blade width

Wind-tunnel investigation of an NACA full-span high-lift lateral-control combination 1: section characteristics, NACA 23012 airfoil

Wind-tunnel investigation of control-surface characteristics 5: the use of a beveled trailing edge to reduce the hinge moment of a control surface

Wind-tunnel investigation of control-surface characteristics 8: a large aerodynamic balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015 airfoil

A flight investigation of short-period longitudinal oscillations of an airplane with free elevator

Flight investigation of the performance and cooling characteristics of a long-nose high-inlet-velocity cowling on the XP-42 airplane

Flight investigation of an NACA ice-detector suitable for use as a rate-of-icing indicator

A flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap

An Experimental Investigation of Flow Across Tube Banks

An Investigation of Hydrofoils in the NACA Tank 1: Effect of Dihedral and Depth of Submersion


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