References: BSCW

shared by CAROL WIESEMAN, updated on Jan 19, 2011

Summary

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

Files

1992021508.pdf
On-line analysis capabilities software
 766.5 KB 188 downloads
NASA_TM104180_BMP.pdf
BMP - Description and Highlights
 918.1 KB 203 downloads
AIAA-1992-2368_Dansberry.pdf
Dyn Characteristics of BSCW
 828.0 KB 184 downloads
AIAA-JA_Vol40_no1_Piatak_OTT.pdf
Oscillating Turntable for the Measurment of Unsteady Aerodynamic Phenomenon (BSCW)
 630.1 KB 261 downloads
AIAA_2002-0171_OTT.pdf
A New Forced Oscillation Capability for the TDT
 522.8 KB 180 downloads
NASA_TM4457_BSCW.pdf
Physical Properties of Benchmark SCW (includes measured coordinates in tables)
 4.8 MB 410 downloads
Schuster_splitterplateTM.pdf
BSCW Splitter Plate Test in TDT
 2.2 MB 146 downloads

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