Coverart for item
The Resource Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches, Charles F. Whitcomb and Harry T. Norton, Jr

Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches, Charles F. Whitcomb and Harry T. Norton, Jr

Label
Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches
Title
Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches
Statement of responsibility
Charles F. Whitcomb and Harry T. Norton, Jr
Creator
Contributor
Subject
Language
eng
Summary
An investigation of the effects of several wing leading-edge modifications on the aerodynamic characteristics of a 45 degree swept-wing fighter-airplane model has been conducted in the Langley 16-foot transonic tunnel at low and high lifting conditions at Mach numbers from 0.85 to 1.03. The investigation included the determination of the effect on longitudinal stability and performance characteristics of wing leading-edge and chord-extension droops of 6 and 20 degrees, chord-extension overhangs of 0.075c and 0.15c (where c is the wing chord), leading-edge notches cut out at the inboard end of the 0.075c chord-extension to depths of 0.075c and 0.125c, and indentation of the model fuselage to conform partially to the supersonic area rule for a Mach number of 1.20. Lift, drag, and pitching-moment data were obtained for configurations with the tail on and off. Comparisons of data obtained from the present model with data from a configuration with leading-edge slats are included
Member of
Cataloging source
OCLCE
http://bibfra.me/vocab/lite/collectionName
Technical Report Archive & Image Library (TRAIL)
http://library.link/vocab/creatorName
Whitcomb, Charles F
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
  • Norton, Harry T.
  • United States
  • Langley Aeronautical Laboratory
Series statement
NACA research memorandum
Series volume
L55H30
http://library.link/vocab/subjectName
  • Airplanes
  • Airplanes
  • Fighter planes
  • Leading edges (Aerodynamics)
  • Aerodynamics, Transonic
  • Wind tunnel testing
  • Charts, diagrams, etc
  • Aerodynamics, Transonic
  • Airplanes
  • Airplanes
  • Charts, diagrams, etc
  • Fighter planes
  • Leading edges (Aerodynamics)
  • Wind tunnel testing
Label
Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches, Charles F. Whitcomb and Harry T. Norton, Jr
Link
Instantiates
Publication
Note
  • Cover title
  • "March 19, 1956."
  • On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publicatiosn Announcements No. 11. Effective Date; December 1, 1959 WHL."
  • NACA Research Memorandum L55H30
Antecedent source
file reproduced from original
Bibliography note
Includes bibliographical references (pages 11-12)
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Dimensions
unknown
Extent
1 online resource (30 pages)
File format
one file format
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Specific material designation
remote
System control number
  • (OCoLC)1014028697
  • (OCoLC)on1014028697
Label
Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches, Charles F. Whitcomb and Harry T. Norton, Jr
Link
Publication
Note
  • Cover title
  • "March 19, 1956."
  • On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publicatiosn Announcements No. 11. Effective Date; December 1, 1959 WHL."
  • NACA Research Memorandum L55H30
Antecedent source
file reproduced from original
Bibliography note
Includes bibliographical references (pages 11-12)
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Dimensions
unknown
Extent
1 online resource (30 pages)
File format
one file format
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Specific material designation
remote
System control number
  • (OCoLC)1014028697
  • (OCoLC)on1014028697

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