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References: BSCW
Benchmark Supercritical Wing was also tested on the OTT with oscillations in Pitch. Only one row of pressure transducers were acquired during these tests. The time histories for this test (548) are available
The Physical Properties of the BSCW (Benchmark Supercritical Wing are provided in
NASA TM 4457 published 1993. Note the previous file that was loaded to this website did not have the tables.
Some results for the test are provided in AIAA 2002-0171 and JOURNAL OF AIRCRAFT article
Complete Metadata
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|---|---|
| accessLevel | public |
| accrualPeriodicity | irregular |
| bureauCode |
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| contactPoint |
{
"fn": "CAROL WIESEMAN",
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"hasEmail": "mailto:carol.d.wieseman@nasa.gov"
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|
| description | <b>Benchmark Supercritical Wing</b> was also tested on the OTT with oscillations in Pitch. Only one row of pressure transducers were acquired during these tests. The time histories for this test (548) are available The Physical Properties of the BSCW (Benchmark Supercritical Wing are provided in <a href="https://c3.ndc.nasa.gov/dashlink/static/media/other/NASA_TM4457_BSCW.pdf"> NASA TM 4457</a> published 1993. Note the previous file that was loaded to this website did not have the tables. Some results for the test are provided in <a href="https://c3.ndc.nasa.gov/dashlink/static/media/other/AIAA_2002-0171_OTT.pdf">AIAA 2002-0171</a> and <a href="https://c3.ndc.nasa.gov/dashlink/static/media/other/AIAA-JA_Vol40_no1_Piatak_OTT.pdf">JOURNAL OF AIRCRAFT article</a> |
| distribution |
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"@type": "dcat:Distribution",
"title": "AIAA_2002-0171_OTT.pdf",
"format": "PDF",
"mediaType": "application/pdf",
"description": "A New Forced Oscillation Capability for the TDT",
"downloadURL": "https://c3.nasa.gov/dashlink/static/media/other/AIAA_2002-0171_OTT.pdf"
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{
"@type": "dcat:Distribution",
"title": "NASA_TM104180_BMP.pdf",
"format": "PDF",
"mediaType": "application/pdf",
"description": "BMP - Description and Highlights",
"downloadURL": "https://c3.nasa.gov/dashlink/static/media/other/NASA_TM104180_BMP.pdf"
},
{
"@type": "dcat:Distribution",
"title": "Schuster_splitterplateTM.pdf",
"format": "PDF",
"mediaType": "application/pdf",
"description": "BSCW Splitter Plate Test in TDT",
"downloadURL": "https://c3.nasa.gov/dashlink/static/media/other/Schuster_splitterplateTM.pdf"
},
{
"@type": "dcat:Distribution",
"title": "AIAA-1992-2368_Dansberry.pdf",
"format": "PDF",
"mediaType": "application/pdf",
"description": "Dyn Characteristics of BSCW",
"downloadURL": "https://c3.nasa.gov/dashlink/static/media/other/AIAA-1992-2368_Dansberry.pdf"
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{
"@type": "dcat:Distribution",
"title": "1992021508.pdf",
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{
"@type": "dcat:Distribution",
"title": "AIAA-JA_Vol40_no1_Piatak_OTT.pdf",
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"description": "Oscillating Turntable for the Measurment of Unsteady Aerodynamic Phenomenon (BSCW)",
"downloadURL": "https://c3.nasa.gov/dashlink/static/media/other/AIAA-JA_Vol40_no1_Piatak_OTT.pdf"
},
{
"@type": "dcat:Distribution",
"title": "NASA_TM4457_BSCW.pdf",
"format": "PDF",
"mediaType": "application/pdf",
"description": "Physical Properties of Benchmark SCW (includes measured coordinates in tables)",
"downloadURL": "https://c3.nasa.gov/dashlink/static/media/other/NASA_TM4457_BSCW.pdf"
}
]
|
| identifier | DASHLINK_293 |
| issued | 2011-01-19 |
| keyword |
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|
| landingPage | https://c3.nasa.gov/dashlink/resources/293/ |
| modified | 2025-04-01 |
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|
| publisher |
{
"name": "Dashlink",
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|
| title | References: BSCW |
