@inproceedings{oai:jaxa.repo.nii.ac.jp:00006559,
 author = {坂上, 博隆 and Sakaue, Hirotaka},
 book = {宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集　第33回・第34回, JAXA Special Publication: Proceedings of the 33rd and 34th JAXA Workshops on Investigation and Control of Boundary-Layer Transition},
 month = {Jan},
 note = {A miniature fluidic oscillator was used to demonstrate the capability of measuring oscillating unsteady aerodynamic fields with 6.4 kHz primary frequency. Pressure maps of various phases were captured by anodized aluminum pressure sensitive paint with platinum (II) meso-tetra (pentafluorolphenyl) porphine as a luminophore. Main uncertainty source comes from fitting the adsorption control model to calibration points and from the pulse width of illumination. The measurement uncertainty of the pressure was 4.65 percent., 資料番号: AA0047776005, レポート番号: JAXA-SP-04-002},
 pages = {13--16},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {陽極酸化皮膜型感圧センサの非定常流への応用},
 volume = {JAXA-SP-04-002},
 year = {2005}
}