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Showing 1 to 20 of 55 for “"Laminar Boundary Layer"”.

  1. Radiative Laminar Boundary Layer Flow

    Chen, Hui-WenUniversity of Illinois at Urbana-Champaign2014

    Made available in DSpace on 2014-12-10T23:36:42Z (GMT). No. of bitstreams: 1 7114699.pdf: 2151244 bytes, checksum: bdfb418c68ea4906fab91099a73491ac (MD5) Previous issue date: 1970

    uiuc Repository record

  2. The laminar boundary layer on spinning bodies of revolution

    Muraca, Ralph JohnVirginia Polytechnic Institute and State University1970

    … and solution of the equations describing the laminar boundary layer on axisymmetric bodies immersed in an oncoming stream and spinning at a constant rate about their axis of revolution. The flow is allowed to be compressible or incompressible and the geometries for which solutions are obtained …

    vt Repository record

  3. Thermal Response Behavior of Laminar Boundary Layer in Wedge Flow

    Chen, James Lin-ShengUniversity of Illinois at Urbana-Champaign2014

    Made available in DSpace on 2014-12-09T17:13:48Z (GMT). No. of bitstreams: 1 7013277.pdf: 9751758 bytes, checksum: 8dd227874e1a1b48556b4f9e0a14104c (MD5) Previous issue date: 1969

    uiuc Repository record

  4. On the stability of the laminar boundary layer between parallel streams

    Lessen, MartinMassachusetts Institute of Technology1948

    Thesis (Sc.D.) Massachusetts Institute of Technology. Dept. of Mechanical Engineering, 1948.

    mit Repository record

  5. Local flowfield about large distributed roughness elements in a laminar boundary layer

    Winkler, John FrancisUniversity of Illinois at Urbana-Champaign2011

    … large roughness elements placed in a flat plate laminar boundary layer was studied. Flowfield measurements were taken upstream, over, and downstream of an isolated hemispherical roughness element and distributed hemispherical roughness elements. The height of the roughness elements was large …

    uiuc Repository record

  6. Thermal Ignition Analysis in the Laminar Boundary Layer Behind a Propagating Shock Front

    Khan, Mushtaq Ahmed2019

    … the ignition of a reactive gas in the laminar boundary layer behind a propagating shock front. The study is based on a one-step, irreversible Arrhenius reaction of a premixed gas; therefore, the ignition phenomenon is thermally induced. The boundary layer consists of a thin, diffusive, …

    odu Repository record

  7. Laminar boundary layer in a partially ionized diatomic gas behind a moving shock

    Moh, Tzu-Chung.Massachusetts Institute of Technology1964

    Thesis: M.S., Massachusetts Institute of Technology, Department of Mechanical Engineering, 1964

    mit Repository record

  8. Forced Convection in Laminar Boundary Layer Over Wedges of Arbitrary Temperature and Flux Distribution

    Cheema, Lakhvendar SinghUniversity of Illinois at Urbana-Champaign2015

    Made available in DSpace on 2015-05-12T22:34:53Z (GMT). No. of bitstreams: 2 license.txt: 4848 bytes, checksum: 96035ab3f5e1c23cc7138a224ce498bd (MD5) 7114698.PDF: 2728892 bytes, checksum: fdb8b598a653c76507ddecae291a1064 (MD5) Previous issue date: 1970

    uiuc Repository record

  9. Second approximations to the solution of laminar boundary layer flow along a flat plate

    Alden, Henry L.Massachusetts Institute of Technology1947

    Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautical Engineering, 1947

    mit Repository record

  10. Stable and high order accurate finite difference method for the incompressible laminar boundary layer equations

    Nchupang, Mojalefa PrinceDepartment of Mechanical Engineering2020

    … high order approximation for the incompressible laminar boundary layer equations. A new set of energystable boundary conditions are derived using the energy method. It is shown that both the weak and strong implementation of these boundary conditions yields an energy estimate. The semidiscrete …

    cape-town Repository record

  11. The laminar boundary layer of a steady, compressible flow in the entrance region of a tube

    Toong, Tau-Yi, 1918-Massachusetts Institute of Technology1951

    Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1951.

    mit Repository record

  12. Solution of the laminar boundary layer of a semi-infinite flat plate given an impulsive change in velocity and temperature

    Bare, Michael DavidVirginia Polytechnic Institute1967

    The laminar boundary layer over a semi-infinite flat plate which is impulsively set in motion in an incompressible fluid and which has a simultaneous step change in surface temperature was studied. An approximate method was derived which can be used to determine the thermal boundary layer thickness …

    vt Repository record

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

    McGowan, John JamesVirginia Polytechnic Institute and State University1970

    … 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 negative …

    vt Repository record

  14. Curvature effects on the stability of three-dimensional laminar boundary layers

    Collier, FayetteVirginia Polytechnic Institute and State University1988

    … disturbances for compressible, three-dimensional laminar boundary layer flow are derived in an orthogonal curvilinear coordinate system. The parallel flow assumption is utilized in the derivation. The system of equations is solved using a finite difference scheme similar to that in a current …

    vt Repository record

  15. Experimental investigation and theoretical considerations of boundary layer transition of the hemisphere at low wall-to-stagnation temperature ratios

    Mayo, Edward E.Virginia Polytechnic Institute1959

    … experimentally whether or not instability of the laminar boundary layer on blunt convex bodies exists when the wall-to-stagnation temperature is lowered. It was found that instability existed and theoretical considerations are given to the transition being associated with the formation of ice on …

    vt Repository record

  16. Hydrodynamic Stability of the boundary layer beneath a Stokes wave

    Giri, GauthamGeorgia Institute of Technology2024

    … to refine the linear stability analysis of the laminar boundary layer beneath a Stokes wave in deep waters, drawing on Fedele’s earlier findings. Fedele’s analysis focused on two-dimensional perturbations and employed a ”momentary” stability criterion. Here, we adopt a comprehensive approach by …

    gatech Repository record

  17. Three dimensional topology and structural differences in the turbulent wake of cantilevered square and circular cylinders protruding thin boundary layers

    Shahroodi, MaryamSchulich School of Engineering2021

    … the effects of the cylinder geometry and the boundary layer state on the wake structures and flow topology. Detailed velocimetry results are presented in the wake of circular and square cylinders protruding a thin laminar boundary layer at a nominal Reynolds number of 10500. The results are …

    calgary Repository record

  18. Numerical Navier-Stokes solutions of supersonic slot injection problems

    Yoon, Sung JoonVirginia Polytechnic Institute and State University1988

    … line Gauss-Seidel relaxation applied to the thin layer Navier-Stokes equations. To test the accuracy of the numerical methods without the complications and uncertainties of turbulence modeling, two sample cases were chosen with laminar flows. The sample problems were the compressible laminar …

    vt Repository record

  19. ΜΕΛΕΤΗ ΤΟΥ ΟΡΙΑΚΟΥ ΣΤΡΩΜΑΤΟΣ ΣΥΜΠΙΕΣΤΟΥ ΡΕΥΣΤΟΥ ΜΕ ΕΦΑΡΜΟΓΗ ΜΑΓΝΗΤΙΚΟΥ ΠΕΔΙΟΥ ΚΑΙ ΕΓΧΥΣΗ ΞΕΝΟΥ ΡΕΥΣΤΟΥ

    Δασκαλάκης, ΙωάννηςΠανεπιστήμιο Πατρών1988

    … A LIGHT FOREIGNGAS (HYDROGEN) IN THE HYPERSONIC LAMINAR BOUNDARY LAYER OF RAREFIED AIR OVER AFLAT PLATE ARE STUDIED. THE VARIABILITY OF THE MIXTURE PROPERTIES WITH TEMPERATURE AND HYDROGEN CONCENTRATION IS TAKEN INTO ACCOUNT. SLIP BOUNDARY CONDITIONSARE PROVIDED TO SIMULATE DEPARTURE FROM THE …

    greece Repository record

  20. High Fidelity Studies in Closed-Loop Control of Unsteady Aerodynamics

    Theobald-Deschine, Miriam

    … control strategy based on POD-ROM focusing on boundary-layer transitional flow in high-fidelity computational studies involving FDL3DI ILES code. Controlling the boundary-layer transition from laminar to turbulent allows the laminar boundary-layer to be lengthened, decreasing skin-friction drag …

    embry-riddle Repository record

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