The Resource Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack, by Deborah Anne Engelmeyer

Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack, by Deborah Anne Engelmeyer

Label
Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack
Title
Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack
Statement of responsibility
by Deborah Anne Engelmeyer
Creator
Language
eng
Related
Cataloging source
UMR
http://library.link/vocab/creatorName
Engelmeyer, Deborah Anne
Degree
M.S.
Dissertation year
1992.
Granting institution
University of Missouri--Rolla
Illustrations
illustrations
Index
no index present
Literary form
non fiction
Label
Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack, by Deborah Anne Engelmeyer
Instantiates
Publication
Carrier category
volume
Carrier category code
  • nc
Carrier MARC source
rdacarrier.
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent.
Control code
26480312
Extent
ix, 113 pages
Media category
unmediated
Media MARC source
rdamedia.
Media type code
  • n
Other physical details
illustrations.
Label
Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack, by Deborah Anne Engelmeyer
Publication
Carrier category
volume
Carrier category code
  • nc
Carrier MARC source
rdacarrier.
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent.
Control code
26480312
Extent
ix, 113 pages
Media category
unmediated
Media MARC source
rdamedia.
Media type code
  • n
Other physical details
illustrations.

Library Locations

    • Curtis Laws Wilson LibraryBorrow it
      400 West 14th Street, Rolla, MO, 65409, US
      37.955220 -91.772210
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