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Oil-flow separation patterns on an ogive forebody
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Keener, E. R. |
| Copyright Year | 1981 |
| Description | Oil flow patterns on a symmetric tangent ogive forebody having a fineness ratio of 3.5 are presented for angles of attack up to 88 deg at a transitional Reynolds number of 8 million (based on base diameter) and a Mach number of 0.25. Results show typical surface flow separation patterns, the magnitude of surface flow angles, and the extent of laminar and turbulent flow for symmetric, asymmetric, and wakelike flow regimes. |
| File Size | 1803649 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820002138 |
| Archival Resource Key | ark:/13960/t3zs7jz3h |
| Language | English |
| Publisher Date | 1981-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aircraft Models Boundary Layer Separation Aerodynamic Configurations Body-wing Configurations Vortices Reynolds Number Flow Distribution Ogives Angle of Attack Separated Flow Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
