Solution Of Non Isoenergetic Supersonic Flows By Method Of Characteristics Volume 3
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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.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1973
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Aeronautics categories.
Flow Field Study About A Hemisphere Cylinder In The Transonic And Low Supersonic Mach Number Range
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Author : T. Hsieh
language : en
Publisher:
Release Date : 1975
Flow Field Study About A Hemisphere Cylinder In The Transonic And Low Supersonic Mach Number Range written by T. Hsieh and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamics, Transonic categories.
A theoretical and experimental study has been conducted of a flow field about a hemisphere-cylinder at zero incidence in the transonic and low supersonic Mach number range (M = 0.7 to 2.0). For M less than or equal to 1, the method used is a combination of the time-dependent solution for the hemispherical nose portion and the method-of-characteristics solution for the cylindrical body portion. The relaxation method has been used for Mach numbers from 0.7 to 1.3. Experimental results indicate a strong interaction of the shock and boundary layer for M approximately equal to 0.8.
Space Shuttle Aerothermodynamics Technology Conference Held At Ames Research Center Moffett Field Calif December 15 16 1971
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Author :
language : en
Publisher:
Release Date : 1972
Space Shuttle Aerothermodynamics Technology Conference Held At Ames Research Center Moffett Field Calif December 15 16 1971 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 Aerothermodynamics categories.
A Directory Of Computer Software Applications Physics 1970 May 1978
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Author : United States. National Technical Information Service
language : en
Publisher:
Release Date : 1978
A Directory Of Computer Software Applications Physics 1970 May 1978 written by United States. National Technical Information Service and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Computer programs categories.
Dynamics Of Compressible Fluids
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Author : Oleksandr Girin
language : en
Publisher: Springer Nature
Release Date : 2022-11-08
Dynamics Of Compressible Fluids written by Oleksandr Girin and has been published by Springer Nature this book supported file pdf, txt, epub, kindle and other format this book has been release on 2022-11-08 with Science categories.
Compressibility is a property inherent in any material, but it does not always manifest itself. Experience suggests that it affects the medium motion only at velocities comparable to the speed of sound. Why do we study compressibility? It turns out that in order to calculate the aircraft streamlining or the internal flow in its engine, or the shell muzzle velocity, or the dynamic load of a shock wave from an accidental blast on a structural element, and in many other cases it is necessary to know and understand the laws of the Dynamics of Compressible Media (DCM) and be able to apply them in practice. This textbook is designed to help readers achieve this goal and learn the basics of DCM. This field of knowledge is high-tech and always focuses on the future: modern developments of hypersonic aircraft, designing more advanced structural elements for airplanes and helicopters, calculating the car aerodynamics, etc. Paradoxes have always given impetus to the search for new technological devices. Unusual effects in DCM include the flow chocking in supersonic outflow from reservoirs (Sect.2.2); the shock wave formation inside an initially smooth flow (Sect.5.3); the generation of a "spallation saucer" of armor inside a tank when a shell hits it (Sect.5.5); the dog-leg of a plane discontinuity surface at shockwave reflection from a rigid wall (Sec.8.1). The way to understand these and other effects is through the creation of quantitative models of a moving compressible fluid.
Development And Application Of The Gim Code For The Cyber 203 Computer
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Author : J. F. Stalnaker
language : en
Publisher:
Release Date : 1982
Development And Application Of The Gim Code For The Cyber 203 Computer written by J. F. Stalnaker and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Geometrical models categories.
U S Government Research Development Reports
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Author :
language : en
Publisher:
Release Date : 1970
U S Government Research Development Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Science categories.
Nasa Contractor Report
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Author :
language : en
Publisher:
Release Date : 1982
Nasa Contractor Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Aeronautics categories.
A Second Order Numerical Method Of Characteristics For Three Dimensional Supersonic Flow Volume 1 Theoretical Development And Results
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Author :
language : en
Publisher:
Release Date : 1969
A Second Order Numerical Method Of Characteristics For Three Dimensional Supersonic Flow Volume 1 Theoretical Development And Results written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with categories.
A new method of characteristics numerical scheme for three-dimensional steady flow has been developed which has second-order accuracy. A complete numerical algorithm for computing internal supersonic flows of the type encountered in ramjet, scramjet or rocket propulsion systems has been developed and programmed for both the IBM 7094 and CDC 6500 computers. The method has been tested for order of accuracy using the exact solution for source flow and Prandtl-Meyer flow. The results of these tests have verified the second-order accuracy of the scheme. Additional accuracy tests using existing methods for solution of two-dimensional axisymmetric flows have shown that the scheme produces accuracies comparable to that of the two-dimensional method of characteristics. The computer program has been used to generate the flow field for several three-dimensional nozzle contours and for nonsymmetric flow into an axisymmetric nozzle. These results reveal the complex natureof three-dimensional flows and the general inadequacy of quasi-three-dimensional analyses which neglect crossflow. An operationally convenient computer program was produced. The program has the capability to analyze nonisoenergetic and nonhomentropic flows of a calorically perfect gas or homentropic flows of a real gas in chemical equilibrium. The initial-value surface options include uniform flow, source flow or axisymmetric tabular data. The nozzle boundary options include conical nozzles, axisymmetric contoured nozzles and super-elliptical nozzles.