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 9 of 9 for “"Three-Dimensional Boundary Layer"”.

  1. Structure and Turbulence of the Three-Dimensional Boundary Layer Flow over a Hill

    Three-dimensional (3D) turbulent boundary layers (TBLs) are ubiquitous in most engineering applications, but most turbulence models used to simulate these flows are built on two-dimensional turbulence theory, limiting the accuracy of simulation results. To improve the accuracy of turbulence …

    vt Repository record for Structure and Turbulence of the Three-Dimensional Boundary Layer Flow over a Hill (opens in a new tab)

  2. A calculation method for the three-dimensional boundary-layer equations in integral form

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992.

    mit Repository record for A calculation method for the three-dimensional boundary-layer equations in integral form (opens in a new tab)

  3. An integral method for quasi three-dimensional boundary layer analysis with rotational effects

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.

    mit Repository record for An integral method for quasi three-dimensional boundary layer analysis with rotational effects (opens in a new tab)

  4. Direct Assessment and Investigation of Nonlinear and Nonlocal Turbulent Constitutive Relations in Three-Dimensional Boundary Layer Flow

    Three-dimensional (3D) turbulent boundary layers (TBLs) play a crucial role in determining the aerodynamic properties of most aero-mechanical devices. However, accurately predicting these flows remains a challenge due to the complex nonlinear and nonlocal physics involved, which makes it difficult …

    vt Repository record for Direct Assessment and Investigation of Nonlinear and Nonlocal Turbulent Constitutive Relations in Three-Dimensional Boundary Layer Flow (opens in a new tab)

  5. Boundary layer flows over sharp and spherically blunted cones at angle of attack to supersonic nonuniform free streams

    … been developed to solve the problem of laminar boundary layers on sharp and spherically blunt cones at angle of attack to nonuniform supersonic free streams. A three-dimensional boundary-layer solution is used to solve sharp cone problems and the afterbody of blunt cone problems. An axisymmetric …

    vt Repository record for Boundary layer flows over sharp and spherically blunted cones at angle of attack to supersonic nonuniform free streams (opens in a new tab)

  6. Development of a numerical method to solve the three-dimensional compressible laminar boundary-layer equations with application to elliptical cones at angle of attack

    A method for solving general compressible three-dimensional boundary-layer flows is developed. The equations are initially placed in a Crocco-type form which makes use of similarity variables. A general solution technique which employs an implicit finite-difference scheme that is stable for …

    vt Repository record for Development of a numerical method to solve the three-dimensional compressible laminar boundary-layer equations with application to elliptical cones at angle of attack (opens in a new tab)

  7. Mean velocity and turbulence measurements of flow around a 6:1 prolate spheroid

    Investigations of the three-dimensional flow around a 6:1 prolate spheroid model 1.37 m long were conducted in the separation and near wake regions along the leeward side. Mean velocity flow field measurements, at α = 10∘ and 15∘ , and at Re = 1.3 x 10⁶ (U<sub>re</sub>= 15.2 mls) and 4.0x 10⁶ …

    vt Repository record for Mean velocity and turbulence measurements of flow around a 6:1 prolate spheroid (opens in a new tab)

  8. Experimental investigation of normal, sonic injection through a wedge-shaped nozzle into supersonic flow

    … was used to determine the size of the three-dimensional boundary layer separation zone in front of each nozzle, and nanoshadowgraph photography was used to visualize the system of shocks and the flow field of each nozzle. Mean flow quantity profiles at several lateral stations were made …

    vt Repository record for Experimental investigation of normal, sonic injection through a wedge-shaped nozzle into supersonic flow (opens in a new tab)

  9. A Basic Three-Dimensional Turbulent Boundary Layer Experiment To Test Second-Moment Closure Models

    In this work, a three-dimensional turbulent boundary layer experiment was set up with alternating stream-wise and span-wise pressure gradients. The pressure gradients are generated as a result of the test section wavy side wall shape. Each side had six sine waves with a trough to peak magnitude to …

    vt Repository record for A Basic Three-Dimensional Turbulent Boundary Layer Experiment To Test Second-Moment Closure Models (opens in a new tab)