The Resource Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range, by Dean R. Chapman

Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range, by Dean R. Chapman

Label
Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range
Title
Airfoil profiles for minimum pressure drag at supersonic velocities
Title remainder
application of shock-expansion theory, including consideration of hypersonic range
Statement of responsibility
by Dean R. Chapman
Creator
Contributor
Author
Issuing body
Subject
Language
eng
Summary
A theoretical investigation is made of airfoil profiles at supersonic velocities to determine the shapes having minimum pressure drag at zero lift for various given auxilliary conditions. Shock-expansion is employed, thereby extending the applicability of the results through the hypersonic range. Curves are presented for Mach numbers of 1.5, 2, 3, 4, 6, 8, and infinity which enable the shape and the drag of an optimum profile to be determined readily if the base pressure is known from experiments. Examples are presented of optimum profiles determined with the aid of experimental base pressure data. Variations in profile shape are investigated to provide information on the degree to which deviations in shape from the optimum can be made without resulting in a significant drag increase
Member of
Action
digitized
Cataloging source
TRAAL
http://bibfra.me/vocab/lite/collectionName
Technical Report Archive & Image Library (TRAIL)
http://library.link/vocab/creatorName
Chapman, Dean R
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary form
non fiction
Nature of contents
  • dictionaries
  • bibliography
http://library.link/vocab/relatedWorkOrContributorName
United States
Series statement
National Advisory Committee for Aeronautics technical note
Series volume
2787
http://library.link/vocab/subjectName
  • Aerodynamic load
  • Aerodynamics, Supersonic
  • Aerofoils
  • Drag (Aerodynamics)
Label
Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range, by Dean R. Chapman
Link
https://texashistory.unt.edu/ark:/67531/metadc56307/
Instantiates
Publication
Note
  • "Ames Aeronautical Laboratory, Moffett Field, California."
  • Title from title screen (viewed June 7, 2019)
  • Date of issue: September 17, 1952
  • Report no. 2787
Bibliography note
Includes bibliographical references (page 24)
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 (44 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
  • (OCoLC)1104148302
  • (OCoLC)on1104148302
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
Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range, by Dean R. Chapman
Link
https://texashistory.unt.edu/ark:/67531/metadc56307/
Publication
Note
  • "Ames Aeronautical Laboratory, Moffett Field, California."
  • Title from title screen (viewed June 7, 2019)
  • Date of issue: September 17, 1952
  • Report no. 2787
Bibliography note
Includes bibliographical references (page 24)
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 (44 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
  • (OCoLC)1104148302
  • (OCoLC)on1104148302
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.

Library Locations

  • Architecture LibraryBorrow it
    Gould Hall 830 Van Vleet Oval Rm. 105, Norman, OK, 73019, US
    35.205706 -97.445050
  • Bizzell Memorial LibraryBorrow it
    401 W. Brooks St., Norman, OK, 73019, US
    35.207487 -97.447906
  • Boorstin CollectionBorrow it
    401 W. Brooks St., Norman, OK, 73019, US
    35.207487 -97.447906
  • Chinese Literature Translation ArchiveBorrow it
    401 W. Brooks St., RM 414, Norman, OK, 73019, US
    35.207487 -97.447906
  • Engineering LibraryBorrow it
    Felgar Hall 865 Asp Avenue, Rm. 222, Norman, OK, 73019, US
    35.205706 -97.445050
  • Fine Arts LibraryBorrow it
    Catlett Music Center 500 West Boyd Street, Rm. 20, Norman, OK, 73019, US
    35.210371 -97.448244
  • Harry W. Bass Business History CollectionBorrow it
    401 W. Brooks St., Rm. 521NW, Norman, OK, 73019, US
    35.207487 -97.447906
  • History of Science CollectionsBorrow it
    401 W. Brooks St., Rm. 521NW, Norman, OK, 73019, US
    35.207487 -97.447906
  • John and Mary Nichols Rare Books and Special CollectionsBorrow it
    401 W. Brooks St., Rm. 509NW, Norman, OK, 73019, US
    35.207487 -97.447906
  • Library Service CenterBorrow it
    2601 Technology Place, Norman, OK, 73019, US
    35.185561 -97.398361
  • Price College Digital LibraryBorrow it
    Adams Hall 102 307 West Brooks St., Norman, OK, 73019, US
    35.210371 -97.448244
  • Western History CollectionsBorrow it
    Monnet Hall 630 Parrington Oval, Rm. 300, Norman, OK, 73019, US
    35.209584 -97.445414
Processing Feedback ...