The Resource Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles, Eugene S. Love

Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles, Eugene S. Love

Label
Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
Title
Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
Statement of responsibility
Eugene S. Love
Creator
Contributor
Subject
Language
eng
Summary
The results of tests of 11 triangular wings were conducted at Mach numbers 1.62, 1.92, and 2.40 to determine the effect of leading-edge shape and to compare actual test values with the nonviscous linear theory. The two series of wings had identical plan forms, a constant thickness ratio of 8 percent, a constant location of maximum-thickness point of 18 percent, and a range of apex half-angles from 10 to 45 degrees. The first series had an elliptical leading edge and the second series, a wedge leading edge. Measurements were made of lift, drag, pitching moment, and pressure distribution, the latter being confined to three wings at one Mach number
Member of
Action
digitized
Cataloging source
OCLCE
http://bibfra.me/vocab/lite/collectionName
Technical Report Archive & Image Library (TRAIL)
http://library.link/vocab/creatorName
Love, Eugene S
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
  • United States
  • Langley Aeronautical Laboratory
  • United States
Series statement
NACA research memorandum
Series volume
L9D07
http://library.link/vocab/subjectName
  • Airplanes
  • Airplanes
  • Airplanes
  • Leading edges (Aerodynamics)
  • Aerodynamics, Supersonic
  • Charts, diagrams, etc
  • Aerodynamics, Supersonic
  • Airplanes
  • Airplanes
  • Airplanes
  • Charts, diagrams, etc
  • Leading edges (Aerodynamics)
Label
Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles, Eugene S. Love
Link
Instantiates
Publication
Note
  • Cover title
  • "May 10, 1949."
  • NACA Research Memorandum L9D07
Antecedent source
file reproduced from original
Bibliography note
Includes bibliographical references
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
Dimensions
unknown
Extent
1 online resource (100 pages)
Form of item
online
Level of compression
  • lossless
  • lossy
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Reformatting quality
  • preservation
  • access
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
  • (OCoLC)885227606
  • (OCoLC)ocn885227606
System details
Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.
Label
Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles, Eugene S. Love
Link
Publication
Note
  • Cover title
  • "May 10, 1949."
  • NACA Research Memorandum L9D07
Antecedent source
file reproduced from original
Bibliography note
Includes bibliographical references
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
Dimensions
unknown
Extent
1 online resource (100 pages)
Form of item
online
Level of compression
  • lossless
  • lossy
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Reformatting quality
  • preservation
  • access
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
  • (OCoLC)885227606
  • (OCoLC)ocn885227606
System details
Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.

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