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Finite element modeling and analysis of Mars entry aeroshell concept /

Bibliographic Details
Main Authors: Ahmed, Samee W. (Author), Lane, Brittney M. (Author)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2017.
Series:NASA technical memorandum ; 2017-219374.
Subjects:
Aerodynamics.
Aeroshells.
Atmospheric entry.
Finite element method.
Lift drag ratio.
Mars atmosphere.
Online Access:https://purl.fdlp.gov/GPO/gpo82527
http://purl.fdlp.gov/GPO/gpo82527
Description
Item Description:"June 2017."
"Performing organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (75 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 53).