The Resource The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow, Chieh-Chien Chang

The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow, Chieh-Chien Chang

Label
The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow
Title
The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow
Statement of responsibility
Chieh-Chien Chang
Creator
Contributor
Author
Issuing body
Subject
Language
eng
Summary
By an extension of Evvard's "diaphragm" concept outside the wing tip, two approximate methods are presented for calculating the aerodynamic behavior of harmonically oscillating, sweptback finite wings with both supersonic leading and trailing edges - one expressing the integration in terms of Fresnal integrals and the second one similar to the first except that a series of expansion of the source-strength function is used. If the wing frequency parameter is small both methods give accurate results in the engineering sense without requiring undue computing skill. A number of graphs are presented to show pressure distribution of the wings at different Mach numbers, sweepback angles, and frequency parameters. Comparisons of pressure coefficients calculated from present methods and exact two dimensional solutions based on linearized theory are made
Member of
Action
digitized
Cataloging source
TRAAL
http://bibfra.me/vocab/lite/collectionName
Technical Report Archive & Image Library (TRAIL)
http://library.link/vocab/creatorName
Zhang, Jieqian
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary form
non fiction
Nature of contents
bibliography
http://library.link/vocab/relatedWorkOrContributorName
  • Johns Hopkins University
  • United States
Series statement
National Advisory Committee for Aeronautics technical note
Series volume
2467
http://library.link/vocab/subjectName
  • Airplanes
  • Oscillating wings (Aerodynamics)
  • Aerodynamics, Supersonic
Label
The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow, Chieh-Chien Chang
Link
https://edit.texashistory.unt.edu/ark:/67531/metadc55838/?q=1100474460
Instantiates
Publication
Note
  • "The Johns Hopkins University."
  • Title from title screen (viewed March 7, 2019)
  • Date of issue: October 1951
  • Report no. 2467
Bibliography note
Includes bibliographical references (page 57)
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Extent
1 online resource (76 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Reproduction note
Electronic reproduction.
System control number
  • (OCoLC)1100474460
  • (OCoLC)on1100474460
System details
Master and use copy. Digital master created according to Technical Guidelines for Digitizing Archival Materials for Electronic Access. U.S. National Archives and Records Administration, 2004.
Label
The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow, Chieh-Chien Chang
Link
https://edit.texashistory.unt.edu/ark:/67531/metadc55838/?q=1100474460
Publication
Note
  • "The Johns Hopkins University."
  • Title from title screen (viewed March 7, 2019)
  • Date of issue: October 1951
  • Report no. 2467
Bibliography note
Includes bibliographical references (page 57)
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Extent
1 online resource (76 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Reproduction note
Electronic reproduction.
System control number
  • (OCoLC)1100474460
  • (OCoLC)on1100474460
System details
Master and use copy. Digital master created according to Technical Guidelines for Digitizing Archival Materials for Electronic Access. U.S. National Archives and Records Administration, 2004.

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