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3 edition of Fast and optimal solution to the "Rankine-Hugoniot problem" found in the catalog.

Fast and optimal solution to the "Rankine-Hugoniot problem"

Fast and optimal solution to the "Rankine-Hugoniot problem"

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Published by National Aeronautics and Space Administration, Goddard Space Flight Center, For sale by the National Technical Information Service in Greenbelt, Md, [Springfield, Va .
Written in English

    Subjects:
  • Astronautics.,
  • Iterative methods (Mathematics)

  • Edition Notes

    Other titlesFast and optimal solution to the Rankine Hugoniot problem.
    StatementAdolfo F. Vinas, Jack D. Scudder.
    SeriesNASA technical memorandum -- 86214.
    ContributionsScudder, Jack D., Goddard Space Flight Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15292318M

    I Daniel Leonard and Ngo van Long () Optimal Control Theory and´ Static Optimization in Economics, Cambridge University Press. I Rangarajan K. Sundaram () A First Course in Optimization Theory, Cambridge University Press. I Morton I. Kamien and Nancy L. Schwartz () Dynamic Optimization, Elsevier - North Holland. McGrawHill. 61 Determining of various asymptotics of solutions of nonlinear time-optimal problems via right ideals in the moment algebra 41 G. M. Sklyar, S. Yu. Ignatovich 41 PM Hybrid Systems 28 L 2-Induced Gains of Switched Linear Systems 45 Jo~ao P. Hespanha 45 48 Is Monopoli’s Model Reference Adaptive Controller Correct? 48 A. S. Morse

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Fast and optimal solution to the "Rankine-Hugoniot problem" Download PDF EPUB FB2

A new, definitive, reliable and fast iterative method is described for determining the geometrical properties of a shock (i.e., θ Bn, n, V s and M A), the conservation constants and the self‐consistent asymptotic magnetofluid variables using the Rankine‐Hugoniot conservation equations.

The technique uses the three dimensional magnetic Cited by: Get this from a library. Fast and optimal solution to the 'Rankine-Hugoniot problem'. [Adolfo F Vinas; Jack D Scudder; Goddard Space Flight Center.].

Fast and optimal solution to the 'Rankine-Hugoniot problem' Authors: Vinas, A. F.; Scudder, J. reliable and fast iterative method is described for determining the geometrical properties of a shock Explicit proof of "uniqueness" of the shock geometry solution by either analytical or graphical methods is given.

The method is applied to. Problem: From the shock-particle velocity plane in Figure 2, draw the curve in the Hugoniot pressure-volume plane. Solution: Let the particle velocity u change from m/s to m/s. As in the last problem, the pressure can be calculated from Eq.

(2), and the ratio of the specific volume across the shock v v1 0/ can be calculated from Size: KB. Rankine-Hugoniot Relations - For steady one-dimensional flow of a combustible gas that burns to completion, equations relating initial and final conditions are readily derived from conservation equations.

- Consider a premixed flammable mixture in a long tube ignited from one end. A combustion wave will travel down the tube starting from. A.F. Viñas, J.D. Scudder, Fast and optimal solution to the Rankine-Hugoniot problem. NASA Memorandum (May ). The classical Rankine-Hugoniot jump conditions, an important cornerstone of modern shock wave physics: ideal assumptions vs.

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The AP Calculus Problem Book Publication history: First edition, Second edition, Third edition, Third edition Revised and Corrected, Fourth edition,Edited by Amy Lanchester Fourth edition Revised and Corrected, Fourth edition, Corrected, This book was produced directly from the author’s LATEX files.

It is in the book: Rational extended thermodynamics - Muller, Ruggeri, In Chapter 8 - Subsection (Weak solutions) and Subsection (Rankine-Hugoniot Equations).

It is given in general terms but it is the proof I was looking for. So the Rankine-Hugoniot condition stays the same in. this book, while randomized rounding [RT87] is presented in Chapter In the primal-dual method for approximation algorithms, an approximate solution to the problem and a feasible solution to the dual of an LP relaxation are constructed simultaneously; the performance guarantee is proved by comparing the values of both solutions.

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A simple ideal Rankine cycle with .