Introduction to Transonic Aerodynamics

Introduction to Transonic Aerodynamics

Author: Roelof Vos

Publisher: Springer

Published: 2015-03-04

Total Pages: 561

ISBN-13: 9401797471

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Written to teach students the nature of transonic flow and its mathematical foundation, this book offers a much-needed introduction to transonic aerodynamics. The authors present a quantitative and qualitative assessment of subsonic, supersonic and transonic flow around bodies in two and three dimensions. The book reviews the governing equations and explores their applications and limitations as employed in modeling and computational fluid dynamics. Some concepts, such as shock and expansion theory, are examined from a numerical perspective. Others, including shock-boundary-layer interaction, are discussed from a qualitative point of view. The book includes 60 examples and more than 200 practice problems. The authors also offer analytical methods such as Method of Characteristics (MOC) that allow readers to practice with the subject matter. The result is a wealth of insight into transonic flow phenomena and their impact on aircraft design, including compressibility effects, shock and expansion waves, shock-boundary-layer interaction and aeroelasticity.


NASA Supercritical Airfoils

NASA Supercritical Airfoils

Author: National Aeronautics and Space Administration (NASA)

Publisher: Createspace Independent Publishing Platform

Published: 2018-07-10

Total Pages: 76

ISBN-13: 9781722660826

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The NASA supercritical airfoil development program is summarized in a chronological fashion. Some of the airfoil design guidelines are discussed, and coordinates of a matrix of family related supercritical airfoils ranging from thicknesses of 2 to 18 percent and over a design lift coefficient range from 0 to 1.0 are presented. Harris, Charles D. Langley Research Center...


Transonic Aerodynamic Characteristics of a Supercritical-wing Transport Model with Trailing-edge Controls

Transonic Aerodynamic Characteristics of a Supercritical-wing Transport Model with Trailing-edge Controls

Author: Michael J. Mann

Publisher:

Published: 1977

Total Pages: 348

ISBN-13:

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The effects of wing trailing-edge control surfaces on the static transonic aerodynamic characteristics of a transport configuration with a supercritical wing were studied. The configuration was tested with both an area-ruled fuselage and a cylindrical fuselage. The Mach number range was from 0.80 to 0.96 and the angle of attack range was from -1 deg to 12 deg. The Reynolds number was 1,580,000 based on the mean aerodynamic chord. Tabular data are presented.