Estimation of nonlinear surface pressure characteristics of aerofoil: A 0-1 test approach
We investigate the nonlinear behaviour of the surface flow over a two-dimensional NACA 2415 airfoil undergoing turbulent inflow having 8.46% TI at Re=3.01×105 using the 0-1 test for chaos. It clearly identifies the overall surface flow changes and also finds the transitions from regular to chaotic b...
保存先:
| 主要な著者: | , , , |
|---|---|
| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
AIP Publishing LLC
2019-05-01
|
| シリーズ: | AIP Advances |
| オンライン･アクセス: | http://dx.doi.org/10.1063/1.5102154 |
| タグ: |
タグなし, このレコードへの初めてのタグを付けませんか!
|