Research Catalog

Finite element modeling and analysis of Mars entry aeroshell concept

Title
Finite element modeling and analysis of Mars entry aeroshell concept / Samee W. Ahmed, Brittney M. Lane.
Author
Ahmed, Samee W.
Publication
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2017.

Available Online

https://purl.fdlp.gov/GPO/gpo82527

Details

Additional Authors
  • Lane, Brittney M.
  • Langley Research Center, issuing body.
Description
1 online resource (75 pages) : color illustrations.
Series Statement
NASA/TM ; 2017-219374
Uniform Title
NASA technical memorandum ; 2017-219374.
Subject
  • Aerodynamics
  • Aeroshells
  • Atmospheric entry
  • Finite element method
  • Lift drag ratio
  • Mars atmosphere
Note
  • "June 2017."
  • "Performing organization: NASA Langley Research Center"--Report documentation page.
Bibliography (note)
  • Includes bibliographical references (page 53).
Type of Report (note)
  • Technical memorandum.
Funding (note)
  • Sponsored by the National Aeronautics and Space Administration
Source of Description (note)
  • Description based on online resource; title from PDF title page (NASA, viewed July 11, 2017)
Call Number
GPO Internet NAS 1.15:2017-219374
OCLC
marcive993430824
Author
Ahmed, Samee W., author.
Title
Finite element modeling and analysis of Mars entry aeroshell concept / Samee W. Ahmed, Brittney M. Lane.
Publisher
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2017.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TM ; 2017-219374
NASA technical memorandum ; 2017-219374.
Bibliography
Includes bibliographical references (page 53).
Type Of Report
Technical memorandum.
Funding
Sponsored by the National Aeronautics and Space Administration 388496.04.01.02
L-20766
Connect to:
https://purl.fdlp.gov/GPO/gpo82527
Added Author
Lane, Brittney M., author.
Langley Research Center, issuing body.
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:2017-219374
View in Legacy Catalog