| タイトル | Status of linear boundary-layer stability and the e to the nth method, with emphasis on swept-wing applications |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800014146 |
| 著者（英） | Hefner, J. N.; Bushnell, D. M. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1980-04-01 |
| 言語 | eng |
| 内容記述 | The-state-of-the-art for the application of linear stability theory and the e to the nth power method for transition prediction and laminar flow control design are summarized, with analyses of previously published low disturbance, swept wing data presented. For any set of transition data with similar stream distrubance levels and spectra, the e to the nth power method for estimating the beginning of transition works reasonably well; however, the value of n can vary significantly, depending upon variations in disturbance field or receptivity. Where disturbance levels are high, the values of n are appreciably below the usual average value of 9 to 10 obtained for relatively low disturbance levels. It is recommended that the design of laminar flow control systems be based on conservative estimates of n and that, in considering the values of n obtained from different analytical approaches or investigations, the designer explore the various assumptions which entered into the analyses. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 80N22633
NASA-TP-1645
L-13313 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/172726 |
