The Resource Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings, by Ken Craig
Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings, by Ken Craig
Resource Information
The item Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings, by Ken Craig represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in University of Missouri-St. Louis Libraries.This item is available to borrow from all library branches.
Resource Information
The item Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings, by Ken Craig represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in University of Missouri-St. Louis Libraries.
This item is available to borrow from all library branches.
- Language
- eng
- Extent
- 37 pages
- Note
-
- Cover title
- At head of title: Joint Institute for Aeronautics and Acoustics
- "September 1991."
- Label
- Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
- Title
- Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
- Statement of responsibility
- by Ken Craig
- Subject
-
- Delta wing airplanes
- Delta wings
- Electronic government information -- United States
- Equilibrium flow
- Flow distribution
- Government publications -- United States
- Grid generation (mathematics)
- Turbulence models
- Unsteady flow (Aerodynamics)
- Upper surface blowing
- Wing profiles
- Airplanes -- Control surfaces
- Language
- eng
- Additional physical form
- Also available via Internet from the NASA Technical Report Server web site. Address as of 4/20/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19920001772%5F1992001772.pdf ; current access is available via PURL.
- Cataloging source
- PIT
- http://library.link/vocab/creatorName
- Craig, Ken
- 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
-
- Joint Institute for Aeronautics and Acoustics
- Ames Research Center
- Series statement
-
- JIAA TR
- NASA CR
- Series volume
-
- 104
- 187979
- http://library.link/vocab/subjectName
-
- Unsteady flow (Aerodynamics)
- Airplanes
- Delta wing airplanes
- Delta wings
- Equilibrium flow
- Flow distribution
- Grid generation (mathematics)
- Turbulence models
- Upper surface blowing
- Wing profiles
- Label
- Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings, by Ken Craig
- Note
-
- Cover title
- At head of title: Joint Institute for Aeronautics and Acoustics
- "September 1991."
- Base of film
- safety base undetermined
- Bibliography note
- Includes bibliographical references (pages 19-20)
- Carrier category
- microfiche
- Carrier category code
-
- he
- Carrier MARC source
- rdacarrier
- Color
- black and white
- Content category
- text
- Content type code
-
- txt
- Content type MARC source
- rdacontent
- Control code
- 34364710
- Dimensions
- 29 cm.
- Dimensions
- 4x6 in. or 11x15 cm.
- Emulsion on film
- diazo
- Extent
- 37 pages
- Form of item
- microfiche
- Generation
- service copy
- Media category
- microform
- Media MARC source
- rdamedia
- Media type code
-
- h
- Other physical details
- illustrations
- http://library.link/vocab/ext/overdrive/overdriveId
- n 92-10990
- Positive negative aspect
- negative
- http://bibfra.me/vocab/marc/reductionRatio
- 02
- ReductionRatioRange
- normal reduction
- Reproduction note
- Microfiche.
- Specific material designation
- microfiche
- Label
- Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings, by Ken Craig
- Note
-
- Cover title
- At head of title: Joint Institute for Aeronautics and Acoustics
- "September 1991."
- Base of film
- safety base undetermined
- Bibliography note
- Includes bibliographical references (pages 19-20)
- Carrier category
- microfiche
- Carrier category code
-
- he
- Carrier MARC source
- rdacarrier
- Color
- black and white
- Content category
- text
- Content type code
-
- txt
- Content type MARC source
- rdacontent
- Control code
- 34364710
- Dimensions
- 29 cm.
- Dimensions
- 4x6 in. or 11x15 cm.
- Emulsion on film
- diazo
- Extent
- 37 pages
- Form of item
- microfiche
- Generation
- service copy
- Media category
- microform
- Media MARC source
- rdamedia
- Media type code
-
- h
- Other physical details
- illustrations
- http://library.link/vocab/ext/overdrive/overdriveId
- n 92-10990
- Positive negative aspect
- negative
- http://bibfra.me/vocab/marc/reductionRatio
- 02
- ReductionRatioRange
- normal reduction
- Reproduction note
- Microfiche.
- Specific material designation
- microfiche
Subject
- Delta wing airplanes
- Delta wings
- Electronic government information -- United States
- Equilibrium flow
- Flow distribution
- Government publications -- United States
- Grid generation (mathematics)
- Turbulence models
- Unsteady flow (Aerodynamics)
- Upper surface blowing
- Wing profiles
- Airplanes -- Control surfaces
Genre
Member of
Library Locations
-
St. Louis Mercantile LibraryBorrow it1 University Blvd, St. Louis, MO, 63121, US38.710138 -90.311107
-
-
University ArchivesBorrow it703 Lewis Hall, Columbia, MO, 65211, US
-
University of Missouri-St. Louis Libraries DepositoryBorrow it2908 Lemone Blvd, Columbia, MO, 65201, US38.919360 -92.291620
-
University of Missouri-St. Louis Libraries DepositoryBorrow it2908 Lemone Blvd, Columbia, MO, 65201, US38.919360 -92.291620
-
Ward E Barnes Education LibraryBorrow it8001 Natural Bridge Rd, St. Louis, MO, 63121, US38.707079 -90.311355
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/portal/Computational-study-of-the-aerodynamics-and/RCkZBtdDKis/" typeof="Book http://bibfra.me/vocab/lite/Item"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/portal/Computational-study-of-the-aerodynamics-and/RCkZBtdDKis/">Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings, by Ken Craig</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/portal/Computational-study-of-the-aerodynamics-and/RCkZBtdDKis/" typeof="Book http://bibfra.me/vocab/lite/Item"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/portal/Computational-study-of-the-aerodynamics-and/RCkZBtdDKis/">Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings, by Ken Craig</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
