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    Advanced Solar Dynamic Space Power Systems, Part II: Detailed Design and Specific Parameters Optimization 

    Source: Journal of Solar Energy Engineering:;1995:;volume( 117 ):;issue: 004:;page 274
    Author(s): A. Agazzani; A. Massardo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aim of this work is the proposal and the analysis of advanced solar dynamic space power systems for electrical space power generation. In the first part of this work (Agazzani and Massardo, ...
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    Advanced Solar Dynamic Space Power Systems, Part I: Efficiency and Surface Optimization 

    Source: Journal of Solar Energy Engineering:;1995:;volume( 117 ):;issue: 004:;page 265
    Author(s): A. Agazzani; A. Massardo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aim of this work is the proposal and the analysis of advanced solar dynamic space power systems for electrical space power generation. The detailed thermodynamic analysis of SDCC (Solar ...
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    Axial Flow Compressor Design Optimization: Part I—Pitchline Analysis and Multivariable Objective Function Influence 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 399
    Author(s): A. Massardo; A. Satta
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design of an axial flow compressor stage has been formulated as a nonlinear mathematical programming problem with the objective of minimizing the aerodynamic losses and the weight of the ...
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    Axial Flow Compressor Design Optimization: Part II—Throughflow Analysis 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 405
    Author(s): A. Massardo; A. Satta; M. Marini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new technique is presented for the design optimization of an axial-flow compressor stage. The procedure allows for optimization of the complete radial distribution of the geometry, since the ...
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    Combined Helium and Combustion Gas Turbine Plant Exploiting Liquid Hydrogen (LH2) Physical Exergy 

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002:;page 257
    Author(s): G. Bisio; A. Massardo; A. Agazzani
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aim of this work is the energy and exergy analysis of a combined plant made up of a conventional gas turbine (heavy-duty or aeroderivative) and a closed helium turbine cycle, which ...
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    Low Area Ratio Aircraft Fuel Jet-Pump Performances With and Without Cavitation 

    Source: Journal of Fluids Engineering:;1992:;volume( 114 ):;issue: 004:;page 626
    Author(s): M. Marini; A. Massardo; A. Satta; M. Geraci
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The experimental analysis performed on several small size low area ratio aircraft fuel jet pumps in JP4 is outlined. The variables investigated were area ratio, nozzle and throat diameters, ...
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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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