The Resource Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base, by Eugene S. Love

Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base, by Eugene S. Love

Label
Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base
Title
Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base
Statement of responsibility
by Eugene S. Love
Creator
Contributor
Author
Issuing body
Subject
Language
eng
Summary
  • An aerodynamic investigation of a slender pointed parabolic body of revolution was conducted at Mach number of 1.92 with and without the effects of an annular supersonic jet exhausting from the base. Measurements with the jet inoperative were made of lift, drag, pitching moment, base pressures, and radial and axial pressures. With the jet in operation, pressure measurements were made over the rear of the body with the primary variables being angle of attack, ratio of jet velocity to stream velocity, and ratio of pressure at jet exit to stream pressure
  • Maximum effects of the jet were obtained at the lower ratio of jet velocity to stream velocity and the highest ratio of jet pressure to stream pressure. These effects amounted to a slight decrease in foredrag, a reduction in lift, and a shift of center of pressure in a destabilizing direction
  • The results with the jet inoperative showed that the radial pressures over the body varied appreciably from the distribution generally employed in most approximate theories. The linearized solutions for lift, pitching moment, and center of pressure gave relatively poor predictions of the ex[erimental results. An analysis of several theoretical methods for calculating pressure distribution and wave drag showed that some methods gave results in considerable disagreement with experimental values
Member of
Action
digitized
Cataloging source
TRAAL
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
  • charts
Index
no index present
Literary form
non fiction
Nature of contents
  • dictionaries
  • bibliography
http://library.link/vocab/relatedWorkOrContributorName
  • United States
  • Langley Aeronautical Laboratory
Series statement
National Advisory Committee for Aeronautics technical note
Series volume
3709
http://library.link/vocab/subjectName
  • Aerodynamic load
  • Aerodynamics, Supersonic
  • Body of revolution
Label
Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base, by Eugene S. Love
Link
https://texashistory.unt.edu/ark:/67531/metadc55995/
Instantiates
Publication
Note
  • "Langley Aeronautical Laboratory, Langley Field, Va."
  • "Supersedes recently declassified NACA Research Memorandum L9K09 by Eugene S. Love, 1950."
  • Title from title screen (viewed June 7, 2019)
  • Date of issue: September 1956
  • Report no. 3709
Bibliography note
Includes bibliographical references (pages 25-26)
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 (62 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations, tables.
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
  • (OCoLC)1104148280
  • (OCoLC)on1104148280
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 investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base, by Eugene S. Love
Link
https://texashistory.unt.edu/ark:/67531/metadc55995/
Publication
Note
  • "Langley Aeronautical Laboratory, Langley Field, Va."
  • "Supersedes recently declassified NACA Research Memorandum L9K09 by Eugene S. Love, 1950."
  • Title from title screen (viewed June 7, 2019)
  • Date of issue: September 1956
  • Report no. 3709
Bibliography note
Includes bibliographical references (pages 25-26)
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 (62 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations, tables.
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
  • (OCoLC)1104148280
  • (OCoLC)on1104148280
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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