| タイトル | Three-Dimensional Boundary-Layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940008600 |
| 著者（英） | Iyer, Venkit |
| 著者所属（英） | Vigyan Research Associates, Inc. |
| 発行日 | 1993-08-01 |
| 言語 | eng |
| 内容記述 | The theory, formulation, and solution of three-dimensional, compressible attached laminar flows, applied to swept wings in subsonic or supersonic flow are discussed. Several new features and modifications to an earlier general procedure described in NASA CR 4269, Jan. 1990 are incorporated. Details of interfacing the boundary-layer computation with solution of the inviscid Euler equations are discussed. A description of the computer program, complete with user's manual and example cases, is also included. Comparison of solutions with Navier-Stokes computations with or without boundary-layer suction is given. Output of solution profiles and derivatives required in boundary-layer stability analysis is provided. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 94N13073
NASA-CR-4531
NAS 1.26:4531 |
| 権利 | No Copyright |
|
