Computation of Separating High Reynolds Number Incompressible Flows Using Uniform Cartesian Grids
Abstract
Most of the research done during the contract period is reported in the "Interim Report" of March, 2002. This is included in section II. Other results, including a breakthrough that has lead to a new, simpler, fully conservative Vorticity Confinement formulation will be discussed in section III. Results of the original formulation for blunt body flow, including comparisons with experiment, are described in section IV. A new, more effective way to treat the surface boundary layer that can be compared with other Vorticity Confinement separation results, such as dynamic stall, is presented in section V. A few of the publications produced during the contract period, which contain relevant material referred to in this report, are included as appendices.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 18, 2002
- Accession Number
- ADA410942
Entities
People
- John Steinhoff
Organizations
- University of Tennessee Space Institute