The Resource Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2, Francis J. Capone ; Langley Research Center, Hampton, Va

Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2, Francis J. Capone ; Langley Research Center, Hampton, Va

Label
Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2
Title
Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2
Statement of responsibility
Francis J. Capone ; Langley Research Center, Hampton, Va
Creator
Contributor
Subject
Language
eng
Member of
Cataloging source
GPO
http://library.link/vocab/creatorName
Capone, Francis J
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary form
non fiction
http://library.link/vocab/relatedWorkOrContributorName
Langley Research Center
Series statement
NASA technical memorandum
Series volume
NASA TM X-3313
http://library.link/vocab/subjectName
  • Airplanes
  • Nozzles
Label
Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2, Francis J. Capone ; Langley Research Center, Hampton, Va
Instantiates
Publication
Note
Cover title
Bibliography note
Bibliography: page 18
Carrier category
volume
Carrier category code
nc
Carrier MARC source
rdacarrier
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Control code
16937948
Dimensions
27 cm.
Extent
1 unnumbered page, 205 pages
Media category
unmediated
Media MARC source
rdamedia
Media type code
n
Other physical details
illustrations
Label
Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2, Francis J. Capone ; Langley Research Center, Hampton, Va
Publication
Note
Cover title
Bibliography note
Bibliography: page 18
Carrier category
volume
Carrier category code
nc
Carrier MARC source
rdacarrier
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Control code
16937948
Dimensions
27 cm.
Extent
1 unnumbered page, 205 pages
Media category
unmediated
Media MARC source
rdamedia
Media type code
n
Other physical details
illustrations

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