Aerodynamics Research

318 books
Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplanceLangley Aeronautical Laboratory
⏱ 58m

Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance

Langley Aeronautical Laboratory

194558 pp.
Frequency of occurrence of atmospheric gusts and of related loads on airplane structuresLangley Aeronautical Laboratory
⏱ 54m

Frequency of occurrence of atmospheric gusts and of related loads on airplane structures

Langley Aeronautical Laboratory

194454 pp.
Note on compressibility effects on downwash at the tail at subcritical speedsLangley Aeronautical Laboratory
⏱ 26m

Note on compressibility effects on downwash at the tail at subcritical speeds

Langley Aeronautical Laboratory

194526 pp.
Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoilLangley Aeronautical Laboratory
⏱ 1h 16m

Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

Langley Aeronautical Laboratory

194576 pp.
Effects on low-speed spray characteristics of various modifications to a powered model of the Boeing XPBB-1 flying boatLangley Aeronautical Laboratory
⏱ 34m

Effects on low-speed spray characteristics of various modifications to a powered model of the Boeing XPBB-1 flying boat

Langley Aeronautical Laboratory

194534 pp.
Electromagnetic-analogy method of solving lifting-surface-theory problemsLangley Aeronautical Laboratory
⏱ 46m

Electromagnetic-analogy method of solving lifting-surface-theory problems

Langley Aeronautical Laboratory

194546 pp.
Recovery corrections for butt-welded, straight-wire thermocouples in high-velocity, high-temperature gas streamsLewis Research Center
⏱ 26m

Recovery corrections for butt-welded, straight-wire thermocouples in high-velocity, high-temperature gas streams

Lewis Research Center

195426 pp.
Method for studying the hunting oscillations of an airplane with a simple type of automatic controlLangley Aeronautical Laboratory
⏱ 26m

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

Langley Aeronautical Laboratory

194426 pp.
Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 651-210 airfoil sectionLangley Aeronautical Laboratory
⏱ 1h 38m

Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 651-210 airfoil section

Langley Aeronautical Laboratory

194598 pp.
Simple method for estimating terminal velocity including effect of compressibility on dragLangley Aeronautical Laboratory
⏱ 28m

Simple method for estimating terminal velocity including effect of compressibility on drag

Langley Aeronautical Laboratory

194528 pp.
Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surfaceLangley Aeronautical Laboratory
⏱ 1h 42m

Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface

Langley Aeronautical Laboratory

1957102 pp.
Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation numberLangley Aeronautical Laboratory
⏱ 36m

Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number

Langley Aeronautical Laboratory

195736 pp.
Theories of turbulenceUnited States.: National Advisory Committee for Aeronautics
⏱ 2h 52m

Theories of turbulence

United States.: National Advisory Committee for Aeronautics

1955172 pp.
Study of the effects of radii of gyration and altitude on aileron effectiveness at high speedLangley Aeronautical Laboratory
⏱ 16m

Study of the effects of radii of gyration and altitude on aileron effectiveness at high speed

Langley Aeronautical Laboratory

194316 pp.
Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speedLangley Aeronautical Laboratory
⏱ 44m

Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed

Langley Aeronautical Laboratory

194444 pp.
Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileronLangley Aeronautical Laboratory
⏱ 24m

Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron

Langley Aeronautical Laboratory

194524 pp.
Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnelLangley Aeronautical Laboratory
⏱ 1h 4m

Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel

Langley Aeronautical Laboratory

194664 pp.
Data for design of entrance vanes from two-dimensional tests of airfoils in cascadeLangley Aeronautical Laboratory
⏱ 1h 0m

Data for design of entrance vanes from two-dimensional tests of airfoils in cascade

Langley Aeronautical Laboratory

194560 pp.
Analysis of available data on the effectiveness of ailerons without exposed overhang balanceLangley Aeronautical Laboratory
⏱ 46m

Analysis of available data on the effectiveness of ailerons without exposed overhang balance

Langley Aeronautical Laboratory

194446 pp.
Airfoil-contour modifications based on [epsilon]-curve method of calculating pressure distributionLangley Aeronautical Laboratory
⏱ 36m

Airfoil-contour modifications based on [epsilon]-curve method of calculating pressure distribution

Langley Aeronautical Laboratory

194436 pp.
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