The Resource Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack, Eldon A. Latham

Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack, Eldon A. Latham

Label
Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack
Title
Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack
Statement of responsibility
Eldon A. Latham
Creator
Contributor
Author
Issuing body
Sponsoring body
Subject
Genre
Language
eng
Member of
Cataloging source
OCLCE
http://library.link/vocab/creatorName
Latham, Eldon A
Funding information
NASA-Ames Research Center
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary form
non fiction
Nature of contents
  • dictionaries
  • bibliography
  • technical reports
http://library.link/vocab/relatedWorkOrContributorName
  • Ames Research Center
  • United States
Series statement
NASA TM
Series volume
X-73118
http://library.link/vocab/subjectName
  • Aerodynamics
  • Jet engines
  • Airplanes
  • Air ducts
  • Supersonic inlets
  • Aerodynamics
  • Mach number
  • Aerodynamics
  • Air ducts
  • Airplanes
  • Jet engines
Type of report
Technical memorandum.
Label
Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack, Eldon A. Latham
Instantiates
Publication
Note
  • "May 1976."
  • Includes appendix
Bibliography note
Includes bibliographical references (page 22)
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Control code
777159342
Extent
1 online resource (79 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
Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack, Eldon A. Latham
Publication
Note
  • "May 1976."
  • Includes appendix
Bibliography note
Includes bibliographical references (page 22)
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Control code
777159342
Extent
1 online resource (79 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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