| タイトル | Pressures Around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent Separation |
| 本文（外部サイト） | http://hdl.handle.net/2060/19990027291 |
| 著者（英） | Lamont, P. J. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1982-11-01 |
| 言語 | eng |
| 内容記述 | This paper reports results From comprehensive pressure tests on an ogive cylinder in the low-turbulence 12-ft pressure wind tunnel at Ames Research Center. The results consist of detailed pressure distributions over a wide range of Reynolds numbers (0.2 x 10(exp 6) to 4.0 x 10(exp 6)) and angles of attack (20 to 90 deg). Most important, the tests encompassed a complete coverage of different roll orientations. This variation of roll orientation is shown to be essential in order to fully define all the possible flow conditions. When the various roll-angle results are combined, it is possible to interpret correctly the effects of changing angle of attack or Reynolds number. Two basic mechanisms for producing asymmetric flow are identified. One mechanism operates in both the laminar and the fully turbulent separation regimes; this mechanism Is the one qualitatively described by the impulsive flow analogy. The other mechanism occurs only in the transitional separation regime. This asymmetric flow has the same form as that found in the two-dimensional cross flow on a circular cylinder in the transitional flow regime. Finally, these results make it possible to draw up critical Reynolds number boundaries between the laminar, transitional, and fully turbulent separation regimes throughout the angle-of-attack range from 20 to 90 deg. |
| NASA分類 | Fluid Mechanics and Heat Transfer |
| レポートNO | NASA/TM-82-208151
AIAA Paper 80-1556R |
| 権利 | No Copyright |
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