Novel Pressure-Sensitive Paint For Cryogenic and Unsteady Wind Tunnel Testing
- 著者名:
- ASAI, K. ( National Aerospace Laboratory )
- AMAO, Y.
- IIJIMA, Y.
- OKURA, I.
- NISHIDE, H.
- 掲載資料名:
- AIAA paper
- シリーズ名:
- AIAA Paper : AIAA Aerodynamic Measurement Technology and Ground Test Conference
- シリーズ巻号:
- 2000
- 発行年:
- 2000
- 通号:
- 2000-2527
- ペーパー番号:
- 00-2527
- 開始ページ:
- 1
- 終了ページ:
- 11
- 出版情報:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- 言語:
- 英語
- 請求記号:
- A07400
- 資料種別:
- テクニカルペーパー
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2
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Evaluation of several calibration techniques for pressure sensitive paint in transonic testing
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Detection of boundary-layer transition in a cryogenic wind tunnel by using luminescent paint
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