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Author : Robert Nelson Hollyer
Publisher :
ISBN 13 :
Total Pages : 174 pages
Book Rating : 4.:/5 (143 download)
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:
Author : J. L. Stollery
Publisher : Chapman & Hall
ISBN 13 :
Total Pages : 936 pages
Book Rating : 4.3/5 (91 download)
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:
Author : Charles E. Treanor
Publisher : SUNY Press
ISBN 13 : 9780873955959
Total Pages : 1130 pages
Book Rating : 4.9/5 (559 download)
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.
Author : Jimmy L. Smith
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.3/5 (121 download)
Download or read book Shock Tube Experiments on Snow written by Jimmy L. Smith and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James V. Zaccor
Publisher :
ISBN 13 :
Total Pages : 222 pages
Book Rating : 4.:/5 (318 download)
Download or read book Procedures for Prediction of Ground Shock Phenomena Based on One-dimensional Shock Propagation Considerations written by James V. Zaccor and published by . This book was released on 1967 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes a definitive experimental study in which shock-induced square-wave pulses in soil were observed to give way to decaying pulse shapes, as in a gas shock tube, and rapid attenuation of peak stress occurred thereafter due to nonlinear propagation in the rarefaction. In the study three different duration pulses were applied to an 8-ft vertical column of granular material confined under boundary conditions leading to a stress-strain (Sigma - Epsilon) behavior described by d to the 2nd power Sigma/d Epsilon to the 2nd power> 0, i.e., a strain-hardening type of response. Applied stresses ranged from 50 to 500 psi. The report describes a simple modification to be applied to the prediction procedure described in the first report of this series in order to take into account, to a first approximation, the nonlinear propagation of unloading waves that occurs in real media because of nonlinear stress-strain behavior in the unloading branch. The procedure which predicts stress and motion histories based on the conservation laws, a measured constitutive relationship, and the applied pressure-time profile, is demonstrated by predicting the entire sequence of an experimentally observed square-wave pulse transformation into a decaying pulse. (Author).
Author : Jack B. Esgar
Publisher :
ISBN 13 :
Total Pages : 732 pages
Book Rating : 4.F/5 ( download)
Download or read book Analytical Study of Soft Landings on Gas-filled Bags written by Jack B. Esgar and published by . This book was released on 1960 with total page 732 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert L. Trimpi
Publisher :
ISBN 13 :
Total Pages : 674 pages
Book Rating : 4.F/5 ( download)
Download or read book A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification written by Robert L. Trimpi and published by . This book was released on 1955 with total page 674 pages. Available in PDF, EPUB and Kindle. Book excerpt: The nonlinear characteristic differential equations applicable to a quasi-one-dimensional unsteady channel flow with friction and heat transfer are linearized and integrated in functional form for the particular study of small perturbations from ideal shock-tube flows. If the equivalence of unsteady- and steady-flow boundary layers is assumed, the problem of determining the perturbation in the unsteady flow reduces to an evaluation of the drag of a flat plate in the equivalent steady flow.
Author : United States. National Aeronautics and Space Administration
Publisher :
ISBN 13 :
Total Pages : 862 pages
Book Rating : 4.3/5 (91 download)
Download or read book NASA Technical Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960 with total page 862 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Aerospace Corporation
Publisher :
ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.E/5 ( download)
Download or read book Test Time in Low Pressure Shock Tubes written by Aerospace Corporation and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Aerospace Corporation
Publisher :
ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.E/5 ( download)
Download or read book Shock Tube Test Time Limitation Due to Turbulent Wall Boundary Layer written by Aerospace Corporation and published by . This book was released on 1963 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 460 pages
Book Rating : 4.3/5 (243 download)
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1958 with total page 460 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : George E. Glawe
Publisher :
ISBN 13 :
Total Pages : 820 pages
Book Rating : 4.F/5 ( download)
Download or read book Experimental Study of Heat Transfer to Small Cylinders in a Subsonic, High-temperature Gas Stream written by George E. Glawe and published by . This book was released on 1957 with total page 820 pages. Available in PDF, EPUB and Kindle. Book excerpt: A Nusselt-Reynolds number relation for cylindrical thermocouple wires in crossflow was obtained from the experimental determination of time constants. Tests were conducted in exhaust gas over a temperature range of 2000 to 3400 R, a Mach number range of 0.3 to 0.8, and a static-pressure range from 2/3 to 1-1/3 atmospheres, yielding a Reynolds number range of 450 to 3000. The correlation obtained is Nu=(0.428 plus or minus 0.003) times the square root of Re with average deviations of a single observation of 8.5 percent. This relation is the same as one previously reported for room-temperature conditions.
Author : N. Muniswamy Reddy
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)
Download or read book Shock-tube Flow Analysis with a Dimensionless Velocity Number written by N. Muniswamy Reddy and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Shock tube flow analysis with dimensionless velocity number.
Author : James F. Roach
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (31 download)
Download or read book Evaluation of an Electromagnetic Shock Tube for Generating Strong Shocks in Air written by James F. Roach and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. Douglas Archer
Publisher :
ISBN 13 :
Total Pages : 780 pages
Book Rating : 4.F/5 ( download)
Download or read book Shock Tubes and Waves written by R. Douglas Archer and published by . This book was released on 1983 with total page 780 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Charles E. Wittliff
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.E/5 ( download)
Download or read book Shock Tube Driver Techniques and Attenuation Measurements written by Charles E. Wittliff and published by . This book was released on 1957 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 500 pages
Book Rating : 4.:/5 (31 download)
Download or read book Technical Note written by and published by . This book was released on 1956 with total page 500 pages. Available in PDF, EPUB and Kindle. Book excerpt:
