Browse TRAIL Inventories

The reduction of aileron operating force by differential linkage

A simplified application of the method of operators to the calculation of disturbed motions of an airplane

A study of the two-control operation of an airplane

Accelerations in Landing with a Tricycle-Type Landing Gear

Operational treatment of the nonuniform-lift theory in airplane dynamics

The influence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts

The Unsteady Lift of a Finite Wing

Transient effects of the wing wake on the horizontal tail

A graphical method of determining pressure distribution in two-dimensional flow

An Analysis of the Stability of an Airplane With Free Controls

Determination of optimum plan forms for control surfaces

Notes on the Stability and Control of Tailless Airplanes

Correction of the Lifting-Line Theory for the Effect of the Chord

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

Theory and preliminary flight tests of an all-movable vertical tail surface

Emergency Measures for Increasing the Range of Fighter Airplanes

Effect of Hinge-Moment Parameters on Elevator Stick Forces in Rapid Maneuvers

Effect of hinge-moment parameters on elevator stick forces in rapid maneuvers

A method for studying the hunting oscillations of an airplane with a simple type of automatic control

A method for studying the hunting oscillations of and airplane with a simple type of automatic control

Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound

Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound

Thin Oblique Airfoils at Supersonic Speed

Thin oblique airfoils at supersonic speed

Wing plan forms for high-speed flight

Flow over a slender body of revolution at supersonic velocities

Wing plan forms for high-speed flight

A Method for Predicting the Stability in Roll of Automatically Controlled Aircraft Based on the Experimental Determination of the Characteristics of an Automatic Pilot

A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot

The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having a Given Lift and a Given Bending Moment

Theory of Wing-Body Drag at Supersonic Speeds


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