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Implementation of Slater Boundary Condition into OVERFLOW

Duncan, Sean

Abstract Details

2013, MS, University of Cincinnati, Engineering and Applied Science: Aerospace Engineering.
Bleed is one of the primary methods of controlling the flow within a mixed compression inlet. In this work the Slater boundary condition, first applied in WindUS, is implemented in OVERFLOW. Further, a simulation using discrete holes is run in order to show the differences between use of the boundary condition and use of the bleed hole geometry. Recent tests at Wright Patterson Air Force Base seek to provide a baseline for study of mixed compression inlets. The inlet used by the Air Force Research Laboratory is simulated in the modified OVERFLOW. The results from the experiment are compared to the CFD to qualitatively assess the accuracy of the simulations. The boundary condition is shown to be robust and viable in studying bleed.
Paul Orkwis, Ph.D. (Committee Chair)
Shaaban Abdallah, Ph.D. (Committee Member)
Mark Turner, Sc.D. (Committee Member)
122 p.

Recommended Citations

Citations

  • Duncan, S. (2013). Implementation of Slater Boundary Condition into OVERFLOW [Master's thesis, University of Cincinnati]. OhioLINK Electronic Theses and Dissertations Center. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1368026265

    APA Style (7th edition)

  • Duncan, Sean. Implementation of Slater Boundary Condition into OVERFLOW. 2013. University of Cincinnati, Master's thesis. OhioLINK Electronic Theses and Dissertations Center, http://rave.ohiolink.edu/etdc/view?acc_num=ucin1368026265.

    MLA Style (8th edition)

  • Duncan, Sean. "Implementation of Slater Boundary Condition into OVERFLOW." Master's thesis, University of Cincinnati, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1368026265

    Chicago Manual of Style (17th edition)