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    A Theory for Strain-Based Structural System Identification 

    Source: Journal of Applied Mechanics:;2001:;volume( 068 ):;issue: 004:;page 521
    Author(s): G. W. Reich; Aerospace Engineer; K. C. Park
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theory for structural system identification which utilizes strains and translational displacements as measured outputs is presented. The state variables of the fundamental first-order form consist ...
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    Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II—Aerodynamic Measurements in the Rotational Frame 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 004:;page 697
    Author(s): Christopher McLean; Boris Glezer; Cengiz Camci; Professor of Aerospace Engineering
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The current paper deals with the aerodynamic measurements in the rotational frame of reference of the Axial Flow Turbine Research Facility (AFTRF) at the Pennsylvania State University. Stationary ...
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    Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 004:;page 687
    Author(s): Christopher McLean; Boris Glezer; Cengiz Camci; Professor of Aerospace Engineering
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The relative aerodynamic and performance effects associated with rotor–NGV gap coolant injections were investigated in the Axial Flow Turbine Research Facility (AFTRF) of the Pennsylvania State ...
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    Experimental Demonstration of Precision Control of a Deployable Optics Structure 

    Source: Journal of Vibration and Acoustics:;2002:;volume( 124 ):;issue: 003:;page 441
    Author(s): R. Scott Erwin; Senior Aerospace Engineer; Karl Schrader; Optical Engineer; Ruth L. Moser; Aerospace Engineer; Steven F. Griffin; Senior Engineer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the development, design, and implementation of a precision control system for a large, sparse-aperture space-deployable telescope testbed. Aspects of the testbed and laboratory ...
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    Predictions of Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions Using an Intermittency Transport Equation 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 003:;page 455
    Author(s): Y. B. Suzen; Senior Engineer Associate; Lennart S. Hultgren; Aerospace Engineer; David E. Ashpis; Aerospace Engineer; P. G. Huang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new transport equation for the intermittency factor was proposed to predict separated and transitional boundary layers under low-pressure turbine airfoil conditions. The intermittent behavior of ...
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    Virtual Skyhook Vibration Isolation System 

    Source: Journal of Vibration and Acoustics:;2002:;volume( 124 ):;issue: 001:;page 63
    Author(s): Steve Griffin; Research Engineer; Joel Gussy; Project Officer; Space Vehicles Directorate; Steven A. Lane; Research Aerospace Engineer; Benjamin K. Henderson; Research Aerospace Engineer; Space Vehicles Directorate; Dino Sciulli; Aerospace Engineer; Space Vehicles Directorate
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This work presents and demonstrates a passive isolation system that offers the performance of a skyhook damper, but without the need of an inertial reference. This “virtual skyhook” isolation ...
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    Analysis of Nonlinear Aeroelastic Panel Response Using Proper Orthogonal Decomposition 

    Source: Journal of Vibration and Acoustics:;2004:;volume( 126 ):;issue: 003:;page 416
    Author(s): Sean A. Mortara; Graduate Research Assistant; Philip Beran; Senior Research Aerospace Engineer; Joseph Slater
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The nonlinear panel flutter problem solved by Dowell in 1966 is used to investigate the new application of the proper orthogonal decomposition model reduction technique to aeroelastic analysis. ...
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    Aerodynamics of Tip Leakage Flows Near Partial Squealer Rims in an Axial Flow Turbine Stage 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 001:;page 14
    Author(s): Cengiz Camci; Professor of Aerospace Engineering; Debashis Dey; Research Assistant; Levent Kavurmacioglu; Visiting Professor
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper deals with an experimental investigation of aerodynamic characteristics of full and partial-length squealer rims in a turbine stage. Full and partial-length squealer rims are investigated ...
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    Large-Eddy Simulation on Curvilinear Grids Using Compact Differencing and Filtering Schemes 

    Source: Journal of Fluids Engineering:;2002:;volume( 124 ):;issue: 004:;page 836
    Author(s): M. R. Visbal; Technical Area Leader; D. P. Rizzetta; Senior Research Aerospace Engineer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This work investigates the application of a high-order finite difference method for compressible large-eddy simulations on stretched, curvilinear and dynamic meshes. The solver utilizes 4th and ...
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    Numerical Study of Nonreacting Gas Turbine Combustor Swirl Flow Using Reynolds Stress Model 

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 003:;page 804
    Author(s): S. L. Yang; R. R. Tacina; Aerospace Engineer; Y. K. Siow; B. D. Peschke
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents recent research on the use of a Reynolds stress turbulence model (RSTM) for three-dimensional flowfield simulation inside gas turbine combustors. It intends to show the ...
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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