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    Simulations of Channel Flows With Effects of Spanwise Rotation or Wall Injection Using a Reynolds Stress Model 

    Source: Journal of Fluids Engineering:;2001:;volume( 123 ):;issue: 001:;page 2
    Author(s): Bruno Chaouat; Senior Scientist
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Simulations of channel flows with effects of spanwise rotation and wall injection are performed using a Reynolds stress model. In this work, the turbulent model is extended for compressible ...
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    Theoretical Modeling of Creep Behavior of Bellows and Some Applications 

    Source: Journal of Pressure Vessel Technology:;2001:;volume( 123 ):;issue: 002:;page 179
    Author(s): Kazuyuki Tsukimori; Senior Scientist
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The use of bellows expansion joints is an effective method to rationalize various piping systems in industry. In the structural design, the requirements for preventing failures such as ratcheting, ...
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    Structure Inclination Angle in a Turbulent Adverse Pressure Gradient Boundary Layer 

    Source: Journal of Fluids Engineering:;2002:;volume( 124 ):;issue: 004:;page 1025
    Author(s): Per-Åge Krogstad; Jon Harald Kaspersen; Senior Scientist
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of a strong adverse pressure gradient on the turbulent structure in an equilibrium boundary layer was studied using two-point space-time correlations. The ρuu correlations from the ...
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    Large-Eddy Simulation of Supersonic Flat-Plate Boundary Layers Using the Monotonically Integrated Large-Eddy Simulation (MILES) Technique 

    Source: Journal of Fluids Engineering:;2002:;volume( 124 ):;issue: 004:;page 868
    Author(s): H. Yan; A. A. Zheltovodov; Senior Scientist; D. Knight
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A supersonic flat-plate boundary layer at a Reynolds number of 2×104 based on the inflow boundary layer thickness is investigated at different Mach numbers (M=2.88 and 4) using the ...
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