Author: Charles D. HarrisPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 80
Book Description
NASA Supercritical Airfoils
Author: Charles D. HarrisPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 80
Book Description
Introduction to Transonic Aerodynamics
Author: Roelof VosPublisher: Springer
ISBN: 9401797471
Category : Technology & Engineering
Languages : en
Pages : 561
Book Description
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 Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 344
Book Description
NASA Technical Paper
Author: NASA Supercritical Airfoils
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722660826
Category :
Languages : en
Pages : 76
Book Description
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...
Wind Tunnels of NASA
Author: Donald D. BaalsPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 218
Book Description
NASA's Contributions to Aeronautics: Aerodynamics, structures, propulsion, controls
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 980
Book Description
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
Transonic Aerodynamic Characteristics of a Supercritical-wing Transport Model with Trailing-edge Controls
Author: Michael J. MannPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 348
Book Description
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.
NASA Technical Memorandum
Author: Aeroacoustics of Flight Vehicles
Author: Harvey H. HubbardPublisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 620
Book Description