The Resource Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0, Jim A. Penland, James B. Hallissy, and James L. Dillon

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0, Jim A. Penland, James B. Hallissy, and James L. Dillon

Label
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
Title
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
Statement of responsibility
Jim A. Penland, James B. Hallissy, and James L. Dillon
Creator
Contributor
Author
Issuing body
Subject
Genre
Language
eng
Member of
Cataloging source
OCLCE
http://library.link/vocab/creatorName
Penland, Jim A
Funding information
Sponsored by National Aeronautics and Space Administration
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
LC call number
TL521.3
LC item number
.N18 no. 1552
Literary form
non fiction
Nature of contents
  • dictionaries
  • bibliography
  • technical reports
http://library.link/vocab/relatedWorkOrContributorName
  • Hallissy, James B.
  • Dillon, James L.
  • United States
  • Langley Research Center
Series statement
NASA technical paper
Series volume
1552
http://library.link/vocab/subjectName
  • Aerodynamics
  • Aerodynamic characteristics
  • Computational fluid dynamics
  • Delta wings
  • Hypersonic aircraft
  • Wind tunnel tests
  • Aerodynamics
Label
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0, Jim A. Penland, James B. Hallissy, and James L. Dillon
Instantiates
Publication
Note
  • Title from title screen (viewed Sept. 22, 2014)
  • "December 1979."
  • "Performing organization, NASA Langley Research Center"--Technical report documentation page
Bibliography note
Includes bibliographical references (pages 20-22)
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Color
black and white
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Control code
761863635
Dimensions
unknown
Extent
1 online resource (144 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Specific material designation
remote
Label
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0, Jim A. Penland, James B. Hallissy, and James L. Dillon
Publication
Note
  • Title from title screen (viewed Sept. 22, 2014)
  • "December 1979."
  • "Performing organization, NASA Langley Research Center"--Technical report documentation page
Bibliography note
Includes bibliographical references (pages 20-22)
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Color
black and white
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Control code
761863635
Dimensions
unknown
Extent
1 online resource (144 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Specific material designation
remote

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