Aerodynamics control of surface shear stress fluctuations in turbulent boundary layers
(eBook)
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Author
Published
Fort Collins, Colo. : Department of Civil Engineering, Colorado State University, 1981.
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Format
eBook
Language
English
Notes
General Note
"CER80-81-VAS46."
General Note
"April 1981."
Bibliography
Includes bibliographical references.
Description
An experimental study of techniques for modifying the surface shear stress, both mean and fluctuating, in turbulent boundary layers is reported. The surface shear along the test section of a 45.7 cm square wind tunnel, with a downstream expansion section, was determined by means of surface-hot-wire-heat-transfer-gauges. Turbulent boundary layers in both zero and adverse pressure gradients were evaluated.
Funding Information
This research was carried out under the Naval Sea Systems Command General Hydromechanics Research Program Subproject,SR 023 01 01.
Funding Information
Administered by the David W. Taylor Naval Ship Research and Development Center, contract,N00014-80-C-0183.
Citations
APA Citation, 7th Edition (style guide)
Sandborn, V. A. (1981). Aerodynamics: control of surface shear stress fluctuations in turbulent boundary layers . Department of Civil Engineering, Colorado State University.
Chicago / Turabian - Author Date Citation, 17th Edition (style guide)Sandborn, Virgil A. 1981. Aerodynamics: Control of Surface Shear Stress Fluctuations in Turbulent Boundary Layers. Department of Civil Engineering, Colorado State University.
Chicago / Turabian - Humanities (Notes and Bibliography) Citation, 17th Edition (style guide)Sandborn, Virgil A. Aerodynamics: Control of Surface Shear Stress Fluctuations in Turbulent Boundary Layers Department of Civil Engineering, Colorado State University, 1981.
MLA Citation, 9th Edition (style guide)Sandborn, Virgil A. Aerodynamics: Control of Surface Shear Stress Fluctuations in Turbulent Boundary Layers Department of Civil Engineering, Colorado State University, 1981.
Note! Citations contain only title, author, edition, publisher, and year published. Citations should be used as a guideline and should be double checked for accuracy. Citation formats are based on standards as of August 2021.
Staff View
Grouped Work ID
417b1f5d-c8a2-a465-db7b-6266dd7dc739-eng
Grouping Information
Grouped Work ID | 417b1f5d-c8a2-a465-db7b-6266dd7dc739-eng |
---|---|
Full title | aerodynamics control of surface shear stress fluctuations in turbulent boundary layers |
Author | sandborn virgil a |
Grouping Category | book |
Last Update | 2022-06-13 10:33:16AM |
Last Indexed | 2024-05-18 00:46:43AM |
Book Cover Information
Image Source | default |
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First Loaded | Jun 30, 2022 |
Last Used | May 17, 2024 |
Marc Record
First Detected | Apr 19, 2018 12:00:00 AM |
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Last File Modification Time | Jul 31, 2021 04:36:53 AM |
MARC Record
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100 | 1 | |a Sandborn, Virgil A. | |
240 | 1 | 0 | |a Aerodynamics (Online) |
245 | 1 | 0 | |a Aerodynamics|h [electronic resource] :|b control of surface shear stress fluctuations in turbulent boundary layers /|c by V.A. Sandborn. |
246 | 3 | |a Aerodynamics, control of surface shear stress fluctuations in turbulent boundary layers | |
246 | 3 | 0 | |a Control of surface shear stress fluctuations in turbulent boundary layers |
264 | 1 | |a Fort Collins, Colo. :|b Department of Civil Engineering, Colorado State University,|c 1981. | |
300 | |a 1 online resource (7 numbered and 26 unnumbered pages) :|b illustrations. | ||
336 | |a text|b txt|2 rdacontent | ||
336 | |a still image|b sti|2 rdacontent | ||
337 | |a computer|b c|2 rdamedia | ||
338 | |a online resource|b cr|2 rdacarrier | ||
490 | 1 | |a CER ;|v 80/81-46 | |
500 | |a "CER80-81-VAS46." | ||
500 | |a "April 1981." | ||
504 | |a Includes bibliographical references. | ||
520 | |a An experimental study of techniques for modifying the surface shear stress, both mean and fluctuating, in turbulent boundary layers is reported. The surface shear along the test section of a 45.7 cm square wind tunnel, with a downstream expansion section, was determined by means of surface-hot-wire-heat-transfer-gauges. Turbulent boundary layers in both zero and adverse pressure gradients were evaluated. | ||
536 | |a This research was carried out under the Naval Sea Systems Command General Hydromechanics Research Program Subproject|f SR 023 01 01. | ||
536 | |a Administered by the David W. Taylor Naval Ship Research and Development Center, contract|b N00014-80-C-0183. | ||
588 | 0 | |a Print version record. | |
650 | 0 | |a Turbulent boundary layer. | |
650 | 0 | |a Aerodynamics. | |
710 | 2 | |a Colorado State University.|b Department of Civil Engineering. | |
776 | 0 | 8 | |i Print version:|a Sandborn, Virgil A.|t Aerodynamics|w (OCoLC)527696758 |
830 | 0 | |a CER ;|v 80/81-46. | |
856 | 4 | 1 | |u http://hdl.handle.net/11629/co:27759_ucsu5132sh31981internet.pdf|z Access online |
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