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 |
|---|---|---|---|
| ACCEPT_osrelease.tar.gz | G-Zipped | Version 1.5 (minor bug fixes) | Open resource |
| accept-introduction-adverse.pdf | Accompanying technical report | Open resource | |
| ACCEPT_osrelease.tar.gz | G-Zipped | Version 1.4 (minor bug fixes) | Open resource |
| 1992021508.pdf | On-line analysis capabilities software | Open resource | |
| AIAA-1992-2368_Dansberry.pdf | Dyn Characteristics of BSCW | Open resource | |
| AIAA_2002-0171_OTT.pdf | A New Forced Oscillation Capability for the TDT | Open resource | |
| AIAA-JA_Vol40_no1_Piatak_OTT.pdf | Oscillating Turntable for the Measurment of Unsteady Aerodynamic Phenomenon (BSCW) | Open resource | |
| NASA_TM104180_BMP.pdf | BMP - Description and Highlights | Open resource | |
| NASA_TM4457_BSCW.pdf | Physical Properties of Benchmark SCW (includes measured coordinates in tables) | Open resource | |
| Schuster_splitterplateTM.pdf | BSCW Splitter Plate Test in TDT | Open resource |