| タイトル | A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone |
| 本文（外部サイト） | http://hdl.handle.net/2060/19960047203 |
| 著者（英） | Selby, Gregory V.; Blanchard, Alan E.; Wilkinson, Stephen P. |
| 著者所属（英） | Old Dominion Univ. |
| 発行日 | 1996-09-01 |
| 言語 | eng |
| 内容記述 | A flared-cone model under adiabatic and cooled-wall conditions was placed in a calibrated, low-disturbance Mach 6 flow and the stability of the boundary layer was investigated using a prototype constant-voltage anemometer. The results were compared with linear-stability theory predictions and good agreement was found in the prediction of second-mode frequencies and growth. In addition, the same 'N = 10' criterion used to predict boundary-layer transition in subsonic, transonic, and supersonic flows under low freestream noise conditions was found to be applicable for the hypersonic flow regime as well. Under cooled-wall conditions, a unique set of spectral data was acquired that documents the linear, nonlinear, and breakdown regions associated with the transition of hypersonic flow under low-noise conditions. |
| NASA分類 | Fluid Mechanics and Heat Transfer |
| レポートNO | 96N32956
NASA-CR-202200
NAS 1.26:202200 |
| 権利 | No Copyright |
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