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    Rotational and Quasiviscous Cold Flow Models for Axisymmetric Hybrid Propellant Chambers 

    Source: Journal of Fluids Engineering:;2010:;volume( 132 ):;issue: 010:;page 101202
    Author(s): Joseph Majdalani; Michel Akiki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this work, we present two simple mean flow solutions that mimic the bulk gas motion inside a full-length, cylindrical hybrid rocket engine. Two distinct methods are used. The first is based ...
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    Explicit Inversion of Stodola’s Area-Mach Number Equation 

    Source: Journal of Heat Transfer:;2011:;volume( 133 ):;issue: 007:;page 71702
    Author(s): Joseph Majdalani; Brian A. Maicke
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Stodola’s area-Mach number relation is one of the most widely used expressions in compressible flow analysis. From academe to aeropropulsion, it has found utility in the design and performance ...
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    Inversion of the Fundamental Thermodynamic Equations for Isentropic Nozzle Flow Analysis 

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 003:;page 31201
    Author(s): Joseph Majdalani; Brian A. Maicke
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The isentropic flow equations relating the thermodynamic pressures, temperatures, and densities to their stagnation properties are solved in terms of the area expansion and specific heat ratios. ...
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    Inception of Turbulence in the Stokes Boundary Layer Over a Transpiring Wall 

    Source: Journal of Fluids Engineering:;2002:;volume( 124 ):;issue: 003:;page 678
    Author(s): Joseph Majdalani; James Barron; Mechanical/Electrical Engineering Department Manager; William K. Van Moorhem
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this work, the onset of turbulence inside a rectangular chamber is investigated, with and without side-wall injection, in the presence of an oscillatory pressure gradient. Two techniques are ...
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