The Resource Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes, by John M. Riebe and Rodger L. Naeseth

Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes, by John M. Riebe and Rodger L. Naeseth

Label
Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes
Title
Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes
Statement of responsibility
by John M. Riebe and Rodger L. Naeseth
Creator
Contributor
Author
Issuing body
Subject
Language
eng
Summary
An investigation was made in the Langley 300-mph 7- by 10-foot tunnel to determine the aerodynamic characteristics of a refined deep-step planing-tail hull with various forebody and afterbody shapes and, for comparison, a streamline body simulating the fuselage of a modern transport airplane. The results of the tests indicated that the configurations incorporating a forebody with a length-beam ratio of 7 had lower minimum drag coefficients that the configurations incorporating a forebody with length-beam raito of 5. The lowest minimum drag coefficients, which were considerably less than that of a conventional hull and slighly less than that of a streamline body, were obtained on the length-beam-ratio-7 forebody, alone and with round center boom. Drag coefficients and longitudinal- and lateral-stability parameters presented include the interference of a 21-percent-thick support wing
Member of
Action
digitized
Cataloging source
TRAAL
http://bibfra.me/vocab/lite/collectionName
Technical Report Archive & Image Library (TRAIL)
http://library.link/vocab/creatorName
Riebe, John M
Government publication
federal national government publication
Illustrations
  • illustrations
  • charts
  • photographs
Index
no index present
Literary form
non fiction
Nature of contents
bibliography
http://library.link/vocab/relatedWorkOrContributorName
  • Naeseth, Rodger L.
  • Langley Aeronautical Laboratory
  • United States
Series statement
National Advisory Committee for Aeronautics technical note
Series volume
2489
http://library.link/vocab/subjectName
  • Seaplanes
  • Seaplanes
  • Planing hulls
  • Stability of airplanes
Label
Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes, by John M. Riebe and Rodger L. Naeseth
Link
https://edit.texashistory.unt.edu/ark:/67531/metadc55709/?q=1100474469
Instantiates
Publication
Note
  • "Langley Aeronautical Laboratory, Langley Field, Va."
  • "Supersedes the recently declassified NACA RM L8F01, 'Aerodynamic Characteristics of a Refined Deep-Step Planing-Tail Flying-Boat Hull with Various Forebody and Afterbody Shapes' by John M. Riebe and Rodger L. Naeseth, 1948."
  • Title from title screen (viewed March 7, 2019)
  • Date of issue: June 1952
  • Report no. 2489
Bibliography note
Includes bibliographical references (page 11)
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 (48 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations, tables, photographs.
Reproduction note
Electronic reproduction.
System control number
  • (OCoLC)1100474469
  • (OCoLC)on1100474469
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
Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes, by John M. Riebe and Rodger L. Naeseth
Link
https://edit.texashistory.unt.edu/ark:/67531/metadc55709/?q=1100474469
Publication
Note
  • "Langley Aeronautical Laboratory, Langley Field, Va."
  • "Supersedes the recently declassified NACA RM L8F01, 'Aerodynamic Characteristics of a Refined Deep-Step Planing-Tail Flying-Boat Hull with Various Forebody and Afterbody Shapes' by John M. Riebe and Rodger L. Naeseth, 1948."
  • Title from title screen (viewed March 7, 2019)
  • Date of issue: June 1952
  • Report no. 2489
Bibliography note
Includes bibliographical references (page 11)
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 (48 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations, tables, photographs.
Reproduction note
Electronic reproduction.
System control number
  • (OCoLC)1100474469
  • (OCoLC)on1100474469
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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