[PDF] Full Symposium On Turbulence 1 July 1949 Download eBook

Report

Author: United States. National Advisory Committee for Aeronautics

Publisher:

Published: 1957

Total Pages: 324

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Technical Note

Author:

Publisher:

Published: 1952

Total Pages: 520

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Technical Note - National Advisory Committee for Aeronautics

Author: United States. National Advisory Committee for Aeronautics

Publisher:

Published: 1955

Total Pages: 886

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Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control

Author: Benjamin Milwitzky

Publisher:

Published: 1955

Total Pages: 348

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Investigation of a Slat in Several Different Positions on an NACA 64A010 Airfoil for a Wide Range of Subsonic Mach Numbers

Author: John A. Axelson

Publisher:

Published: 1954

Total Pages: 696

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An investigation of the two-dimensional aerodynamic characteristics of an NACA 64A010 airfoil with a slat has been conducted in the Mach number range from 0.25 to 0.85, with a corresponding Reynolds number range from 3.4 million to 8.1 million. Two families of slat positions were investigated, one with the slat leading edge extended forward along the airfoil chord line, and the other with the slat extended forward and displaced below the chord line.