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Active control of instabilities in laminar boundary-layer flow. part 1: an overview
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Erlebacher, Gordon Joslin, Ronald D. Hussaini, M. Yousuff |
| Copyright Year | 1994 |
| Description | This paper (the first in a series) focuses on using active-control methods to maintain laminar flow in a region of the flow in which the natural instabilities, if left unattended, lead to turbulent flow. The authors review previous studies that examine wave cancellation (currently the most prominent method) and solve the unsteady, nonlinear Navier-Stokes equations to evaluate this method of controlling instabilities. It is definitely shown that instabilities are controlled by the linear summation of waves (i.e., wave cancellation). Although a mathematically complete method for controlling arbitrary instabilities has been developed (but not yet tested), the review, duplication, and physical explanation of previous studies are important steps for providing an independent verification of those studies, for establishing a framework for subsequent work which will involve automated transition control, and for detailing the phenomena by which the automated studies can be used to expand knowledge of flow control. |
| File Size | 1120793 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950012543 |
| Archival Resource Key | ark:/13960/t2q57j06r |
| Language | English |
| Publisher Date | 1994-12-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Navier-stokes Equation Laminar Boundary Layer Wave Attenuation Laminar Flow Tollmien-schlichting Waves Boundary Layer Transition Boundary Layer Stability Active Control Boundary Layer Control Boundary Layer Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |