Cfl3d Users Manual Version 50
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Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : |
Release | : 1999* |
Genre | : |
ISBN | : |
Download CFL3D User's Manual (Version 5.0)... NASA/TM-1998-208444... Oct. 26, 1998 Book in PDF, Epub and Kindle
Author | : Sherrie L. Krist |
Publisher | : |
Total Pages | : 376 |
Release | : 1998 |
Genre | : |
ISBN | : |
Download CFL3D User's Manual (Version 5.0) Book in PDF, Epub and Kindle
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 370 |
Release | : 2018-07-23 |
Genre | : |
ISBN | : 9781723538308 |
Download Cfl3d User's Manual (Version 5.0) Book in PDF, Epub and Kindle
This document is the User's Manual for the CFL3D computer code, a thin-layer Reynolds-averaged Navier-Stokes flow solver for structured multiple-zone grids. Descriptions of the code's input parameters, non-dimensionalizations, file formats, boundary conditions, and equations are included. Sample 2-D and 3-D test cases are also described, and many helpful hints for using the code are provided. Krist, Sherrie L. and Biedron, Robert T. and Rumsey, Christopher L. Langley Research Center NASA/TM-1998-208444, NAS 1.15:208444, L-17702 RTOP 522-31-61-02...
Author | : Sherrie Lynn Krist |
Publisher | : |
Total Pages | : 0 |
Release | : 1998 |
Genre | : Computational fluid dynamics |
ISBN | : |
Download CFL3D User's Manual Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1144 |
Release | : 1999 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, Epub and Kindle
Author | : Bernhard Eisfeld |
Publisher | : Springer |
Total Pages | : 106 |
Release | : 2015-03-24 |
Genre | : Technology & Engineering |
ISBN | : 331915639X |
Download Differential Reynolds Stress Modeling for Separating Flows in Industrial Aerodynamics Book in PDF, Epub and Kindle
This book presents recent progress in the application of RANS turbulence models based on the Reynolds stress transport equations. A variety of models has been implemented by different groups into different flow solvers and applied to external as well as to turbo machinery flows. Comparisons between the models allow an assessment of their performance in different flow conditions. The results demonstrate the general applicability of differential Reynolds stress models to separating flows in industrial aerodynamics.
Author | : |
Publisher | : |
Total Pages | : 166 |
Release | : 1999 |
Genre | : |
ISBN | : |
Download NASA Langley Scientific and Technical Information Output: 1998 Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 650 |
Release | : 2004 |
Genre | : Aeronautics |
ISBN | : |
Download AIAA Aerospace Sciences Meeting and Exhibit, 42nd Book in PDF, Epub and Kindle
Author | : Daniel G. Baize |
Publisher | : |
Total Pages | : 810 |
Release | : 1999 |
Genre | : High-speed aeronautics |
ISBN | : |
Download 1997 NASA High-Speed Research Program Aerodynamic Performance Workshop Book in PDF, Epub and Kindle
Author | : John E. Lamar |
Publisher | : |
Total Pages | : 170 |
Release | : 2001 |
Genre | : Airplanes |
ISBN | : |
Download Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds Book in PDF, Epub and Kindle
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.