| タイトル | Investigation of Separation and the Associated Heat-Transfer and Pressure Distribution on Cone-Cylinder-Flare Configurations |
| 本文（外部サイト） | http://hdl.handle.net/2060/20150019680 |
| 著者（英） | Ferguson, Harold; Schaefer, John W. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1962-01-01
1962 |
| 言語 | eng |
| 内容記述 | The separated region across the cylinder-flare junction of a conecylinder-flare configuration and its effect on the overall heat-transfer and pressure distributions were investigated at a Mach number of 4.98. Results are presented for pure laminar and transitional separation and for both laminar and turbulent attached flow on a 15 deg half-angle cone-cylinder model with conical flare afterbodies of 10 deg, 17 deg, 24 deg, and. 56 deg half-angles. The free-stream unit Reynolds number ranged from l.6x10(sup 6)to 5.5x(sup 6) ft(sup -1)and the wall temperature from T(sub w/T(sub aw) = 0.18 to 1.0. The extent of a pure laminar separation and a transitional separation was found to decrease with wall cooling, decreasing flare angle, and increasing unit Reynolds number. The heat transfer at reattachment and downstream was dependent on the type of separation - pure laminar or transitional. Low heat-transfer rates were found downstream of a pure laminar separation. For transitional separation, the heat transfer downstream of reattachment was at the high values associated with a thin turbulent boundary layer, with peak heating in the vicinity of reattachment. |
| NASA分類 | Fluid Mechanics and Thermodynamics; Aerodynamics |
| レポートNO | E-1404 |
| 権利 | No Copyright |
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