| Автор | Joslin, Ronald D. |
| Дата выпуска | 1998 |
| dc.description | ▪ Abstract Aircraft laminar flow control (LFC) from the 1930s through the 1990s is reviewed and the current status of the technology is assessed. Examples are provided to demonstrate the benefits of LFC for subsonic and supersonic aircraft. Early studies related to the laminar boundary-layer flow physics, manufacturing tolerances for laminar flow, and insect-contamination avoidance are discussed. LFC concept studies in wind-tunnel and flight experiments are the major focus of the paper. LFC design tools are briefly outlined for completeness. |
| Формат | application.pdf |
| Издатель | Annual Reviews |
| Копирайт | Annual Reviews |
| Название | AIRCRAFT LAMINAR FLOW CONTROL <sup>1</sup> |
| DOI | 10.1146/annurev.fluid.30.1.1 |
| Print ISSN | 0066-4189 |
| Журнал | Annual Review of Fluid Mechanics |
| Том | 30 |
| Первая страница | 1 |
| Последняя страница | 29 |
| Аффилиация | Joslin, Ronald D.; Fluid Mechanics and Acoustics Division, NASA Langley Research Center, Hampton, Virginia 23681-0001; e-mail: R.D.Joslin@larc.nasa.gov |
