A Study of Attenuation in the Shock Tube

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Publisher :
ISBN 13 :
Total Pages : 174 pages
Book Rating : 4.:/5 (143 download)

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Book Synopsis A Study of Attenuation in the Shock Tube by : Robert Nelson Hollyer

Download or read book A Study of Attenuation in the Shock Tube written by Robert Nelson Hollyer and published by . This book was released on 1953 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube with Hydrogen and Helium as Driver Gases

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ISBN 13 :
Total Pages : 716 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube with Hydrogen and Helium as Driver Gases by : Jim J. Jones

Download or read book Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube with Hydrogen and Helium as Driver Gases written by Jim J. Jones and published by . This book was released on 1957 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation has been made of the attenuation of strong shock waves in air in a shock tube. Time-history measurements were made of the static pressure at several stations in the wall of the tube. The internal diameter of the tube is 3.75 inches. shock-wave-velocity data were taken for a distance along the tube of about 120 feet.

Experimental Shock Tube Study of Attenuation of Weak Shock Wave

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ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.:/5 (132 download)

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Book Synopsis Experimental Shock Tube Study of Attenuation of Weak Shock Wave by : Raymond D. Heinrich (MAJ, USAF.)

Download or read book Experimental Shock Tube Study of Attenuation of Weak Shock Wave written by Raymond D. Heinrich (MAJ, USAF.) and published by . This book was released on 1972 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Study of Shock Wave Attenuation in a Five Centimer Square Shock Tube

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ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.:/5 (2 download)

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Book Synopsis A Study of Shock Wave Attenuation in a Five Centimer Square Shock Tube by : Charles Eugene Fuller

Download or read book A Study of Shock Wave Attenuation in a Five Centimer Square Shock Tube written by Charles Eugene Fuller and published by . This book was released on 1967 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, Or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison

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ISBN 13 :
Total Pages : 682 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, Or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison by : Robert L. Trimpi

Download or read book A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, Or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison written by Robert L. Trimpi and published by . This book was released on 1958 with total page 682 pages. Available in PDF, EPUB and Kindle. Book excerpt: The linearized attenuation theory of NACA Technical Note 3375 is modified in the following manner: (a) an unsteady compressible local skin-friction coefficient is employed rather than the equivalent steady-flow incompressible coefficient; (b) a nonlinear approach is used to permit application of the theory to large attenuations; and (c) transition effects are considered. Curves are presented for predicting attenuation for shock pressure ratios up to 20 and a range of shock-tube Reynolds numbers. Comparison of theory and experimental data for shock wave strengths between 1.5 and 10 over a wide range of Reynolds numbers shows good agreement with the nonlinear theory evaluated for a transition Reynolds nuniber of 2.5 million.

Shock Tube Study of Attenuation of Air Flow Through Chokes (U).

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ISBN 13 :
Total Pages : 35 pages
Book Rating : 4.:/5 (623 download)

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Book Synopsis Shock Tube Study of Attenuation of Air Flow Through Chokes (U). by : Suffield Experimental Station

Download or read book Shock Tube Study of Attenuation of Air Flow Through Chokes (U). written by Suffield Experimental Station and published by . This book was released on 1965 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Shock Wave Velocity Attenuation in a Shock Tube

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ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (19 download)

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Book Synopsis Shock Wave Velocity Attenuation in a Shock Tube by : Bobby Luther McDaniel

Download or read book Shock Wave Velocity Attenuation in a Shock Tube written by Bobby Luther McDaniel and published by . This book was released on 1967 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Shock Tube Research: Proceedings of the Eighth International Shock Tube Symposium, Imperial College, London, 5-8 July 1971

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Publisher : Chapman & Hall
ISBN 13 :
Total Pages : 936 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Shock Tube Research: Proceedings of the Eighth International Shock Tube Symposium, Imperial College, London, 5-8 July 1971 by : J. L. Stollery

Download or read book Shock Tube Research: Proceedings of the Eighth International Shock Tube Symposium, Imperial College, London, 5-8 July 1971 written by J. L. Stollery and published by Chapman & Hall. This book was released on 1971 with total page 936 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effect of Radiation on Shock Velocity Attenuation in Electromagnetic Shock Tubes

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ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis The Effect of Radiation on Shock Velocity Attenuation in Electromagnetic Shock Tubes by : John Alexander Thornton

Download or read book The Effect of Radiation on Shock Velocity Attenuation in Electromagnetic Shock Tubes written by John Alexander Thornton and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: OBSERVATIONS ARE REPORTED IN A STUDY OF EFFECTS OF RADIATION ON SHOCK VELOCITY ATTENUATION IN THE CONICAL ELECTROMAGNETIC SHOCK TUBE. A summary is included of findings which have appeared in the literature along with the approximate blast wave theory, which has become the primary method of making theoretical velocity attenuation calculations. These published observations lead to the question of the effect of radiation on the velocity attenuation in a tube with highly reflective walls such as might be employed in a propulsion system. The approximate blast wave theory is then adapted in developing a modified approximate method for calculating the effect of radiation on shock velocity attenuation. Approximate radiation equations are combined with the velocity attenuation equations and a study is made of factors which might influence the velocity attenuation by radiation. It is concluded that radiation will be an important factor only for strong shocks moving into a dense gas (approximately 1/10 atmosphere or greater and room temperature). A description of the electromagnetic shock tube is given, and some of the velocity attenuation experiments which are being conducted are discussed. No attenuation due to radiation has been noted. These experiments conducted at low velocities and densities thus agree with the predictions of the approximate blast wave theory modified to account for radiation effects. (Author).

Attenuation in a Shock Tube Due to Unsteady-boundary-layer Action

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (671 download)

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Book Synopsis Attenuation in a Shock Tube Due to Unsteady-boundary-layer Action by : Harold Mirels

Download or read book Attenuation in a Shock Tube Due to Unsteady-boundary-layer Action written by Harold Mirels and published by . This book was released on 1954 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for obtaining the attenuation of a shock wave in a shock tube due to the unsteady boundary layer along the shock-tube walls. It is assumed that the boundary layer is thin relative to the tube diameter and induces one-dimensional longitudinal pressure waves whose strength is proportional to the vertical velocity at the edge of the boundary layer. The contributions of the various regions in a shock tube to shock attenuation are indicated.

Attenuation in the Shock Tube

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Attenuation in the Shock Tube by : Robert N. Hollyer

Download or read book Attenuation in the Shock Tube written by Robert N. Hollyer and published by . This book was released on 1956 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Study of Shock Wave Attenuation in Tunnels

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ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.:/5 (267 download)

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Book Synopsis A Study of Shock Wave Attenuation in Tunnels by : Robert O. Clark

Download or read book A Study of Shock Wave Attenuation in Tunnels written by Robert O. Clark and published by . This book was released on 1962 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical investigation of shock wave expansion and viscous attenuation in a tunnel is described. In particular, relationships between the applied and transmitted shock pressure are presented for various entrance configurations and orientations. Shock tube data are given to verify the theory. Working equations and graphs are given to aid in the solution of other shock wave-tunnel problems, assuming a classical wave form for the shock wave and a constant tunnel cross-section.

Attenuation of the Shock in a Shock Tube Due to the Effect of Wall Boundary Layer

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ISBN 13 :
Total Pages : 11 pages
Book Rating : 4.:/5 (46 download)

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Book Synopsis Attenuation of the Shock in a Shock Tube Due to the Effect of Wall Boundary Layer by : G. F. Anderson

Download or read book Attenuation of the Shock in a Shock Tube Due to the Effect of Wall Boundary Layer written by G. F. Anderson and published by . This book was released on 1968 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Shock Tubes and Waves

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Publisher : SUNY Press
ISBN 13 : 9780873955959
Total Pages : 1130 pages
Book Rating : 4.9/5 (559 download)

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Book Synopsis Shock Tubes and Waves by : Charles E. Treanor

Download or read book Shock Tubes and Waves written by Charles E. Treanor and published by SUNY Press. This book was released on 1982-01-01 with total page 1130 pages. Available in PDF, EPUB and Kindle. Book excerpt: Proceedings from a symposium on shock tubes and waves held July 6-9, 1981.

The Effect of Viscous Attenuation on Shock Tube Performance

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ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.:/5 (328 download)

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Book Synopsis The Effect of Viscous Attenuation on Shock Tube Performance by : Nick Roger McKenzie

Download or read book The Effect of Viscous Attenuation on Shock Tube Performance written by Nick Roger McKenzie and published by . This book was released on 1994 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Attenuation of the Shock in a Shock Tube Due to the Effect of Wall Boundary Layer

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (747 download)

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Book Synopsis Attenuation of the Shock in a Shock Tube Due to the Effect of Wall Boundary Layer by : Gordon Francis Anderson

Download or read book Attenuation of the Shock in a Shock Tube Due to the Effect of Wall Boundary Layer written by Gordon Francis Anderson and published by . This book was released on 1966 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effect of Wall Friction on the Strength of Shock Waves in Tubes and Hydraulic Jumps in Channels

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Effect of Wall Friction on the Strength of Shock Waves in Tubes and Hydraulic Jumps in Channels by : Coleman duP. Donaldson

Download or read book The Effect of Wall Friction on the Strength of Shock Waves in Tubes and Hydraulic Jumps in Channels written by Coleman duP. Donaldson and published by . This book was released on 1949 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theory is presented for the attenuation due to viscous boundary layer of shock waves traveling in closed passages. Because of the similar nature of the problem, the theory is also developed for the attenuation of a hydraulic jump moving in a channel. The results of experiments that bear out the theory are presented for both a shock tube and a hydraulic channel.