References: BSCW

Description

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

Resources

Name Format Description Link
33 BMP - Description and Highlights https://c3.nasa.gov/dashlink/static/media/other/NASA_TM104180_BMP.pdf
33 A New Forced Oscillation Capability for the TDT https://c3.nasa.gov/dashlink/static/media/other/AIAA_2002-0171_OTT.pdf
33 BSCW Splitter Plate Test in TDT https://c3.nasa.gov/dashlink/static/media/other/Schuster_splitterplateTM.pdf
33 Dyn Characteristics of BSCW https://c3.nasa.gov/dashlink/static/media/other/AIAA-1992-2368_Dansberry.pdf
33 On-line analysis capabilities software https://c3.nasa.gov/dashlink/static/media/other/1992021508.pdf
33 Oscillating Turntable for the Measurment of Unsteady Aerodynamic Phenomenon (BSCW) https://c3.nasa.gov/dashlink/static/media/other/AIAA-JA_Vol40_no1_Piatak_OTT.pdf
33 Physical Properties of Benchmark SCW (includes measured coordinates in tables) https://c3.nasa.gov/dashlink/static/media/other/NASA_TM4457_BSCW.pdf
33 Accompanying technical report https://c3.nasa.gov/dashlink/static/media/algorithm/accept-introduction-adverse.pdf
19 Version 1.4 (minor bug fixes) https://c3.nasa.gov/dashlink/static/media/algorithm/ACCEPT_osrelease.tar.gz
19 Version 1.5 (minor bug fixes) https://c3.nasa.gov/dashlink/static/media/ACCEPT_osrelease_2.tar.gz

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  • dashlink
  • nasa
  • ames

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