| タイトル | The Development and Implementation of a Cryogenic Pressure Sensitive Paint System in the National Transonic Facility |
| 本文（外部サイト） | http://hdl.handle.net/2060/20090007697 |
| 著者（英） | Goad, William K.; Massey, Edward A.; Goodman, Kyle Z.; Goad, Linda R.; Oglesby, Donald M.; Leighty, Bradley D.; Lipford, William E.; Watkins, A. Neal |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2009-01-05 |
| 言語 | eng |
| 内容記述 | The Pressure Sensitive Paint (PSP) method was used to measure global surface pressures on a model at full-scale flight Reynolds numbers. In order to achieve these conditions, the test was carried out at the National Transonic Facility (NTF) operating under cryogenic conditions in a nitrogen environment. The upper surface of a wing on a full-span 0.027 scale commercial transport was painted with a porous PSP formulation and tested at 120K. Data was acquired at Mach 0.8 with a total pressure of 200 kPa, resulting in a Reynolds number of 65 x 106/m. Oxygen, which is required for PSP operation, was injected using dry air so that the oxygen concentration in the flow was approximately 1535 ppm. Results show qualitative agreement with expected results. This preliminary test is the first time that PSP has been successfully deployed to measure global surface pressures at cryogenic condition in the NTF. This paper will describe the system as installed, the results obtained from the test, as well as proposed upgrades and future tests. |
| NASA分類 | Chemistry and Materials (General) |
| レポートNO | LF99-8224 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
|
