The Resource Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers, A. B. Blair, Jr. ; Langley Research Center, Hampton, Va

Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers, A. B. Blair, Jr. ; Langley Research Center, Hampton, Va

Label
Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers
Title
Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers
Statement of responsibility
A. B. Blair, Jr. ; Langley Research Center, Hampton, Va
Creator
Contributor
Subject
Language
eng
Member of
Cataloging source
GPO
http://library.link/vocab/creatorName
Blair, A. B
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
  • Langley Research Center
  • United States
Series statement
NASA technical memorandum ; NASA TM X-3376
http://library.link/vocab/subjectName
  • Aerodynamics, Supersonic
  • Airplanes
  • Stability of space vehicles
Label
Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers, A. B. Blair, Jr. ; Langley Research Center, Hampton, Va
Instantiates
Publication
Note
Cover title
Bibliography note
Bibliography: page 9
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
16940252
Dimensions
27 cm.
Extent
1 unnumbered page, 95 pages
Media category
unmediated
Media MARC source
rdamedia
Media type code
n
Other physical details
illustrations
Label
Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers, A. B. Blair, Jr. ; Langley Research Center, Hampton, Va
Publication
Note
Cover title
Bibliography note
Bibliography: page 9
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
16940252
Dimensions
27 cm.
Extent
1 unnumbered page, 95 pages
Media category
unmediated
Media MARC source
rdamedia
Media type code
n
Other physical details
illustrations

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