Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 4 of 4 for “"Shock Wave/Boundary Layer Interaction (SBLI)"”.

  1. Evaluation of a displacement-body model for hypersonic shock-wave/boundary-layer interaction

    … thesis, a displacement-body model for strong-interaction shock-wave/boundary-layer interaction (SBLI) is presented and evaluated. The model considers 2-D flow over a flat plate with an adiabatic wall. The separation bubble is modeled as a displacement body with constant surface pressure, the …

    mit Repository record for Evaluation of a displacement-body model for hypersonic shock-wave/boundary-layer interaction (opens in a new tab)

  2. The relationship between surface geometry and transonic intake performance during off-design climb

    … However, these designs often have a stronger shock on the windward front-lip of the intake during off-design climb, producing a severe shock wave--boundary-layer interaction (SBLI) that greatly increases the ingested incompressible boundary-layer displacement thickness, \(\delta_i^*\), and …

    cambridge Repository record for The relationship between surface geometry and transonic intake performance during off-design climb (opens in a new tab)

  3. Sidewall effects in compression corner shock-wave/boundary-layer interactions

    … inlets and research wind tunnels. When a shock wave boundary layer interaction (SBLI) occurs in a rectangular cross sectioned duct, the streamwise corner flows tend to separate, resulting in highly three-dimensional behaviour in the sidewall region. These corner separations have been seen …

    cambridge Repository record for Sidewall effects in compression corner shock-wave/boundary-layer interactions (opens in a new tab)

  4. Numerical and experimental investigation of VG flow control for a low-boom inlet

    The application of vortex generators (VGs) for shock/boundary layer interaction flow control in a novel external compression, axisymmetric, low-boom concept inlet was studied using numerical and experimental methods. The low-boom inlet design features a zero-angle cowl and relaxed isentropic …

    uiuc Repository record for Numerical and experimental investigation of VG flow control for a low-boom inlet (opens in a new tab)