Characteristic Calculation Of Non Equilibrium Flows
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Characteristic Calculation Of Non Equilibrium Flows
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Author : R. Sedney
language : en
Publisher:
Release Date : 1962
Characteristic Calculation Of Non Equilibrium Flows written by R. Sedney and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Nonequilibrium thermodynamics categories.
Characteristic Calculation Of Non Equilibrium Flows
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Author : Raymond Sedney
language : en
Publisher:
Release Date : 1962
Characteristic Calculation Of Non Equilibrium Flows written by Raymond Sedney and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Nonequilibrium thermodynamics categories.
Solution Of Non Isoenergetic Supersonic Flows By Method Of Characteristics Volume 3
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Author :
language : en
Publisher:
Release Date : 1972
Solution Of Non Isoenergetic Supersonic Flows By Method Of Characteristics Volume 3 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.
Airfoil Characteristics In A Nonequilibrium Ambient Stream Based On Linearized Theory
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Author : James Joe Der
language : en
Publisher:
Release Date : 1964
Airfoil Characteristics In A Nonequilibrium Ambient Stream Based On Linearized Theory written by James Joe Der and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aerofoils categories.
Airfoil Characteristics In A Nonequilibrium Ambient Stream Based On Linearized Theory
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Author : James J. Der
language : en
Publisher:
Release Date : 1964
Airfoil Characteristics In A Nonequilibrium Ambient Stream Based On Linearized Theory written by James J. Der and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aerofoils categories.
The aerodynamic characteristics of a lifting body in a nonequilibrium stream are studied for a simple case, namely, the case of a nonequilibrium oncoming stream past a thin airfoil at a small angle of attack. Analytical solutions are obtained by the use of nonequilibrium linearized theory. Results show that when the relaxation length on the indward side of the airfoil is not appreciably different from that on the leeward side, a nonequilibrium ambient condition will normally induce a higher pressure and lower drag, but will not affect the lift, pitching moment, and the center of pressure. The local nonequilibrium condition behind the leading-edge shock, on the other hand, will affect all of the aerodynamic characteristics in general. When the relaxation length on the windward side is significantly different from that on the leeward side, on the other hand, the nonequilibrium ambient condition will also affect the lift, pitching moment, and the center of the pressure. In general, the higher the suction on the leeward side gives higher lift and larger pitching moment because the condition on the leeward side is closer to frozen.
The High Temperature Aspects Of Hypersonic Flow
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Author : Wilbur C. Nelson
language : en
Publisher: Elsevier
Release Date : 2014-12-02
The High Temperature Aspects Of Hypersonic Flow written by Wilbur C. Nelson and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-12-02 with Science categories.
The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
Similitude For Normal Shock Waves In Nonequilibrium Flows
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Author : Ralph E. Thomas
language : en
Publisher:
Release Date : 1965
Similitude For Normal Shock Waves In Nonequilibrium Flows written by Ralph E. Thomas and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Shock waves categories.
Similarity parameters are developed which govern the length of nonequilibrium zones behind normal shock waves. Non-equilibrium effects produced by both vibrational relaxation and dissociation are considered. The parameters can also account for arbitrary levels of free-stream vibrational energy or dissociation level. The validity of the parameters is examined using numerical computations of the properties of the non-equilibrium fields. These computations are made with the aid of experimentally based rate expressions. The parameters, when written in a form describing the variation of non-equilibrium zone length with Mach number, are shown to have acceptable accuracy. (Author).
Theoretical Studies Of Supersonic Two Dimensional And Axisymmetric Nonequilibrium Flow Including Calculations Of Flow Through A Nozzle
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Author : James Joe Der
language : en
Publisher:
Release Date : 1963
Theoretical Studies Of Supersonic Two Dimensional And Axisymmetric Nonequilibrium Flow Including Calculations Of Flow Through A Nozzle written by James Joe Der and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aerodynamics, Supersonic categories.
Chemical and vibrational nonequilibrium phenomena in steady inviscid flow fields are studied by the analysis of flow past curved boundaries. Possible alternative choices of the state variables to be used are considered. General features of the nonequilibrium flow are studied by examination of the mathematical properties of the nonlinear flow equations. An axisymmetric nonequilibrium flow of air through a supersonic nozzle is analyzed by means of numerical computations. The coupling effects between nonuniformity (across a nozzle section) and nonequilibrium, not taken into account in the quasi-one-dimensional flow approximation, are revealed by the present analysis.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1974
Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aeronautics categories.
Nonequilibrium Flows
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Author : Peter P. Wegener
language : en
Publisher:
Release Date : 1969
Nonequilibrium Flows written by Peter P. Wegener and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Air flow categories.