A Critique of High-performance Shock Tube Driving Techniques PDF Download
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Author: Walter R. Warren
Publisher:
ISBN:
Category :
Languages : en
Pages : 56
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Book Description
The various high-performance shock tube driving techniques considered have been grouped as high pressure/high speed of sound conventional drivers, electric and magnetic field interaction drivers, detonation drivers, and those that derive their flow characteristics from the coupling of energy addition and wave processes in an unconventional manner. 'High performance' can be taken to refer to any property of a shock tube flow that is important to a particular study: for example, shock velocity, driven gas temperature, pressure, and density levels, driven gas kinetic to static energy ratio, and uniformity and duration of the driven gas flow. Data from recent references are compared to determine the relative effectiveness of different driving techniques and the predictability of flow properties. Several fluid dynamic problem areas are outlined; requirements for their study in shock driven facilities are discussed and compared with capabilities resulting from the use of various driving techniques. (Author).
Author: Walter R. Warren
Publisher:
ISBN:
Category :
Languages : en
Pages : 56
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Book Description
The various high-performance shock tube driving techniques considered have been grouped as high pressure/high speed of sound conventional drivers, electric and magnetic field interaction drivers, detonation drivers, and those that derive their flow characteristics from the coupling of energy addition and wave processes in an unconventional manner. 'High performance' can be taken to refer to any property of a shock tube flow that is important to a particular study: for example, shock velocity, driven gas temperature, pressure, and density levels, driven gas kinetic to static energy ratio, and uniformity and duration of the driven gas flow. Data from recent references are compared to determine the relative effectiveness of different driving techniques and the predictability of flow properties. Several fluid dynamic problem areas are outlined; requirements for their study in shock driven facilities are discussed and compared with capabilities resulting from the use of various driving techniques. (Author).
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892
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Book Description
Author: Irving Israel Glass
Publisher: University of Toronto Press
ISBN: 1487597584
Category : Education
Languages : en
Pages : 852
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Book Description
This volume contains the proceedings of a symposium held at the University of Toronto in June 1969. The symposium consisted of six sessions; each containing an invited paper, followed by six contributed papers reporting on recent, relevant research and development. The topics are: a review of research problems in basic shock tube flows and the possibilities for the shock tube in the future; driving techniques; explosive drivers; theoretical and experimental research in electromagnetic shock tubes; chemical kinetics and spectroscopy; and a review of shock tube diagnostics, instrumentation and fundamental data as well as the measurement of physical quantities.
Author: I. I. Glass
Publisher:
ISBN:
Category :
Languages : en
Pages : 850
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Book Description
Contents: Basic flows; High-performance driving techniques; Explosive drivers; Electromagnetic shock tubes; Spectroscopy and kinetics; and Diagnostics and data.
Author: J. L. Stollery
Publisher:
ISBN:
Category : Shock tubes
Languages : en
Pages : 998
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Book Description
Author: I. I. Glass
Publisher: [Toronto, Ont.] : University of Toronto Press
ISBN:
Category : Shock tubes
Languages : en
Pages : 860
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Book Description
Author: J. L. Stollery
Publisher: Chapman & Hall
ISBN:
Category : Science
Languages : en
Pages : 936
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Book Description
Author: BALLMAN
Publisher: Springer Science & Business Media
ISBN: 1461203791
Category : Technology & Engineering
Languages : en
Pages : 448
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Book Description
These three volumes entitled Advances in Hypersonics contain the Proceedings of the Second and Third Joint US/Europe Short Course in Hypersonics which took place in Colorado Springs and Aachen. The Second Course was organized at the US Air Force Academy, USA in January 1989 and the Third Course at Aachen, Germany in October 1990. The main idea of these Courses was to present to chemists, com puter scientists, engineers, experimentalists, mathematicians, and physicists state of the art lectures in scientific and technical dis ciplines including mathematical modeling, computational methods, and experimental measurements necessary to define the aerothermo dynamic environments for space vehicles such as the US Orbiter or the European Hermes flying at hypersonic speeds. The subjects can be grouped into the following areas: Phys ical environments, configuration requirements, propulsion systems (including airbreathing systems), experimental methods for external and internal flow, theoretical and numerical methods. Since hyper sonic flight requires highly integrated systems, the Short Courses not only aimed to give in-depth analysis of hypersonic research and technology but also tried to broaden the view of attendees to give them the ability to understand the complex problem of hypersonic flight. Most of the participants in the Short Courses prepared a docu ment based on their presentation for reproduction in the three vol umes. Some authors spent considerable time and energy going well beyond their oral presentation to provide a quality assessment of the state of the art in their area of expertise as of 1989 and 1991.
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 528
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Book Description
Author: N. Muniswamy Reddy
Publisher:
ISBN:
Category : Measurement
Languages : en
Pages : 28
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Book Description
Shock tube flow analysis with dimensionless velocity number.
