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PLOT3D User's Manual

PLOT3D User's Manual PDF Author:
Publisher:
ISBN:
Category : Computer graphics
Languages : en
Pages : 308

Book Description


PLOT3D User's Manual

PLOT3D User's Manual PDF Author:
Publisher:
ISBN:
Category : Computer graphics
Languages : en
Pages : 308

Book Description


PEGSUS 4.0 User's Manual

PEGSUS 4.0 User's Manual PDF Author: N. E. Suhs
Publisher:
ISBN:
Category : Computational fluid dynamics
Languages : en
Pages : 238

Book Description
Many aerodynamic configurations are too complex to be represented by a single computational mesh. A multiple-mesh domain decomposition method called chimera has been developed to allow complex aerodynamic configurations to be modeled by a system of individually generated meshes, each representing a component of the overall configuration. The chimera approach requires the use of two computer codes, PEGSUS and a flow solver. PEGSUS calculates the interactions among the meshes and produces a file consisting of interpolation information that is used by the flow solver to obtain a global flow-field solution for the entire mesh system. This report documents the design and use of the latest version (4.0) of PEGSUS, and describes techniques for proper modeling of complex aerodynamic configurations.

An Introductory Guide to Scientific Visualization

An Introductory Guide to Scientific Visualization PDF Author: Rae Earnshaw
Publisher: Springer Science & Business Media
ISBN: 3642581013
Category : Computers
Languages : en
Pages : 170

Book Description
Scientific visualization is concerned with exploring data and information insuch a way as to gain understanding and insight into the data. This is a fundamental objective of much scientific investigation. To achieve this goal, scientific visualization utilises aspects in the areas of computergraphics, user-interface methodology, image processing, system design, and signal processing. This volume is intended for readers new to the field and who require a quick and easy-to-read summary of what scientific visualization is and what it can do. Written in a popular andjournalistic style with many illustrations it will enable readers to appreciate the benefits of scientific visualization and how current tools can be exploited in many application areas. This volume is indispensible for scientists and research workers who have never used computer graphics or other visual tools before, and who wish to find out the benefitsand advantages of the new approaches.

Solid Modeling Aerospace Research Tool (SMART) User's Guide, Version 2.0

Solid Modeling Aerospace Research Tool (SMART) User's Guide, Version 2.0 PDF Author:
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 108

Book Description


Tecplot, Version 7 User's Manual

Tecplot, Version 7 User's Manual PDF Author:
Publisher:
ISBN:
Category : Computer graphics
Languages : en
Pages : 500

Book Description


PLOT3D User's Manual

PLOT3D User's Manual PDF Author:
Publisher:
ISBN:
Category : Computer graphics
Languages : en
Pages : 302

Book Description


Graphics Mini Manual

Graphics Mini Manual PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

Book Description


Technology 2001

Technology 2001 PDF Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 548

Book Description


Technology 2000

Technology 2000 PDF Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 436

Book Description


Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds

Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds PDF Author: John E. Lamar
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 170

Book Description
Geometrical, flight, computational fluid dynamics (CFD), and wind-tunnel studies for the F-16XL-1 airplane are summarized over a wide range of test conditions. Details are as follows: (1) For geometry, the upper surface of the airplane and the numerical surface description compare reasonably well. (2) For flight, CFD, and wind-tunnel surface pressures, the comparisons are generally good at low angles of attack at both subsonic and transonic speeds; however, local differences are present. In addition, the shock location at transonic speeds from wind-tunnel presure contours is near the aileron hinge line and generally is in correlative agreement with flight results.