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Bücher von Langley Aeronautical Laboratory

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Wind-tunnel Investigation of Control-surface Characteristics.

Author: Langley Aeronautical Laboratory

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Charts for the Minimum-weight Design of 24S-T Aluminum-alloy Flat Compression Panels With Longitudinal Z-section Stiffeners

Author: Langley Aeronautical Laboratory

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Numerical Evaluation of the Wake-survey Equations for Subsonic Flow Including the Effect of Energy Addition

Author: Langley Aeronautical Laboratory

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Wind-tunnel Tests of a Blunt-nose Aileron With Beveled Trailing Edge on an NACA 66(215)-216 Airfoil With Several Modifications of Aileron Nose and Adjacent Airfoil Contour

Author: Langley Aeronautical Laboratory

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Theory of Propellers.

Author: Langley Aeronautical Laboratory

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Flight Tests of the Lateral Control Characteristics of an F6F-3 Airplane Equipped With Spring-tab Ailerons

Author: Langley Aeronautical Laboratory

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Flight Measurements of the Rudder Control and Sideslip Characteristics of Four Vertical Tail Arrangements on the P-40 Series Airplanes

Author: Langley Aeronautical Laboratory

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Some Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave Drag

Author: Langley Aeronautical Laboratory

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Summary of Information on Support Interference at Transonic and Supersonic Speeds

Author: Langley Aeronautical Laboratory

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Theoretical Determination of Low-drag Supercavitating Hydrofoils and Their Two-dimensional Characteristics at Zero Cavitation Number

Author: Langley Aeronautical Laboratory

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Wind-tunnel Investigation of Control-surface Characteristics.

Author: Langley Aeronautical Laboratory

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Flight Studies of the Horizontal-tail Loads Experienced by a Modern Pursuit Airplane in Abrupt Maneuvers

Author: Langley Aeronautical Laboratory

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Flight Investigation of NACA Aileron Modifications for the Improvement of the Lateral Control Characterisitcs of a High-speed Fighter Airplance

Author: Langley Aeronautical Laboratory

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Effect of Mach Number on Position Error as Applied to a Pitot-static Tube Located 0.55 Chord Ahead of an Airplane Wing

Author: Langley Aeronautical Laboratory

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Exploratory Investigation of Transpiration Cooling of a 40° Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures of 1,295° to 2,910° F

Author: Langley Aeronautical Laboratory

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Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel

Author: Langley Aeronautical Laboratory

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Wind-tunnel Investigation of Effects of a Pusher Propeller on Lift, Profile Drag, Pressure Distribution, and Boundary-layer Transition of a Flapped Wing

Author: Langley Aeronautical Laboratory

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Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel

Author: Langley Aeronautical Laboratory

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Determination of the Stability and Control Characteristics of a Straight-wing, Tailless Fighter-airplane Model in the Langley Free-flight Tunnel

Author: Langley Aeronautical Laboratory

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Theory of Propellers.

Author: Langley Aeronautical Laboratory

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