Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques /

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Bibliographic Details
Author / Creator:Jones, Kenneth M., author.
Imprint:[Washington, D.C.] : National Aeronautics and Space Administration, [1995]
Description:1 online resource (25 pages) : illustrations.
Language:English
Series:NASA-TM ; 112005
NASA technical memorandum ; 112005.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/11288384
Hidden Bibliographic Details
Other authors / contributors:Biedron, Robert T., author.
Whitlock, Mark, author.
American Institute of Aeronautics and Astronautics.
United States. National Aeronautics and Space Administration, issuing body.
Notes:"13th Applied Aerodynamics Conference June 19-22, 1995, San Diego, California."
"AIAA 95-1855."
Includes bibliographical references (page 12).
Description based on online resource; title from PDF title page (NASA, viewed June 22, 2017).
Other form:Print version: Application of a navier-stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques
Microfiche version: Jones, Kenneth M. Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:112005

MARC

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504 |a Includes bibliographical references (page 12). 
588 |a Description based on online resource; title from PDF title page (NASA, viewed June 22, 2017). 
500 |a "AIAA 95-1855." 
650 7 |a Aerodynamic configurations.  |2 nasat 
650 7 |a Airfoils.  |2 nasat 
650 7 |a Computational fluid dynamics.  |2 nasat 
650 7 |a Navier-Stokes equation.  |2 nasat 
650 7 |a Reynolds number.  |2 nasat 
650 7 |a Wing flaps.  |2 nasat 
650 7 |a Aerofoils.  |2 fast  |0 http://id.worldcat.org/fast/fst00798241 
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