Shock Tube Test Time Limitation Due to Turbulent Wall Boundary Layer PDF Download
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Author: Aerospace Corporation
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 72
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Book Description
Shock tube test time limitation due to the premature arrival of the contact surface is analytically investigated for wholly turbulent wall boundary layers. The results are compared with those for wholly laminar wall boundary layers. Working curves are presented for more accurate estimates of test time in specific cases. (Author) -- NTRL website.
Author: Aerospace Corporation
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 72
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Book Description
Shock tube test time limitation due to the premature arrival of the contact surface is analytically investigated for wholly turbulent wall boundary layers. The results are compared with those for wholly laminar wall boundary layers. Working curves are presented for more accurate estimates of test time in specific cases. (Author) -- NTRL website.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 542
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Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 652
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 78
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Book Description
Author: S. N. B. Murthy
Publisher: AIAA
ISBN: 9781600863912
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 558
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Book Description
Annotation Leading researchers provide a cohesive treatment of the complex issues in high-speed propulsion, as well as introductions to the current capabilities for addressing several fundamental aspects of high-speed vehicle propulsion development. Includes more than 380 references, 290 figures and tables, and 185 equations.
Author: Krishnan Radhakrishnan
Publisher:
ISBN:
Category : Chemical kinetics
Languages : en
Pages : 160
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Book Description
Author: Irving Israel Glass
Publisher: University of Toronto Press
ISBN: 1487597584
Category : Education
Languages : en
Pages : 983
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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:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 656
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Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1148
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Author: Jet Propulsion Laboratory (U.S.)
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 646
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Book Description
