Langley Aeronautical Laboratory

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Investigation of effect of sideslip on lateral stability characteristics.: I, circular fuselage with variations in vertical-tail area and tail length with and without horizontal tail surface

by Langley Aeronautical Laboratory
First published in 1944 — 3 editions
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Theory of propellers.: I, Determination of the circulation function and the mass coefficient for dual-rotating propellers

by Langley Aeronautical Laboratory
First published in 1944 — 3 editions
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Wind-Tunnel Investigation of Control-surface Characteristics: XXII, Medium and Large Aerodynamic Balances of Two Nose Shapes and a Plain Overhang Used with a 0. 20-Airfoil-chord Flap on an NACA 0009 Airfoil

by Langley Aeronautical Laboratory First published in 2021 — 2 editions

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Theory of Propellers: III, the Slipstream Contraction with Numerical Values for Two-Blade and Four-blade Propellers

by Langley Aeronautical Laboratory First published in 2023 — 2 editions

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Theory of Propellers: I, Determination of the Circulation Function and the Mass Coefficient for Dual-Rotating Propellers

by Langley Aeronautical Laboratory First published in 2021 — 2 editions

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Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel

by Langley Aeronautical Laboratory First published in 1944 — 2 editions
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Hinge moments of sealed-internal-balance arrangements for control surfaces.: II, experimental investigation of fabric seals in the presence of a thin-plate overhang

by Langley Aeronautical Laboratory
First published in 1945 — 2 editions
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Summary of Available Knowledge Concerning Skin Friction and Heat Transfer and Its Application to the Design of High-Speed Missiles

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-flight Tunnel

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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Effect of the Lift Coefficient on Propeller Flutter

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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Flight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered with Camouflage Paint

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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Supersonic-Tunnel Tests of Projectiles in Germany and Italy

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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Pressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2. 05, 2. 54, And 2. 04

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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Heat Transfer and Pressure Measurement on a 5-Inch Hemispherical Concave Nose at a Mach Number Of 2. 0

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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General Solutions of Optimum Problems in Nonstationary Flight

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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Correlation of Supersonic Convective Heat-Transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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Hinge Moments of Sealed-Internal-balance Arrangements for Control Surfaces: I, Theoretical Investigation

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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Experimental Determination of the Effect of Negative Dihedral on Lateral Stability and Control Characteristics at High Lift Coefficients

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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

by Langley Aeronautical Laboratory First published in 2021 — 1 edition

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OLID: OL9964631A

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Created December 23, 2021
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December 23, 2021

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Langley Aeronautical Laboratory

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