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RTO-TR-26
Computational Unsteady Aerodynamics computer codes are being increasingly used. In order to
validate their results they must be tested against valid experimental data. The present report aims at
collecting reliable experimental data on unsteady aerodynamics and presenting them in a form
which permits use for verification of codes. For ease of handling, the data are also presented in
machine readable form (CD-ROM). Data on increasingly complex generic forms were selected and
the following categories are covered: flutter, buffet, stability and control, dynamic stall, cavity
flows, store separation. Computational solutions are included in order to permit evaluation of codes
and analysis of solutions which differ from experimental data.
Complete Metadata
| bureauCode |
[ "026:00" ] |
|---|---|
| identifier | DASHLINK_289 |
| issued | 2011-01-12 |
| landingPage | https://c3.nasa.gov/dashlink/resources/289/ |
| programCode |
[ "026:029" ] |
