RTO-TR-26

Description

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.

Resources

Name Format Description Link
33 RTO-TR-026 Entire document https://c3.nasa.gov/dashlink/static/media/publication/TR-026-ALL.pdf

Tags

  • dashlink
  • nasa
  • ames

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