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Shock Tube Test Time Limitation Due To Turbulent Wall Boundary Layer
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Book Synopsis Shock Tube Test Time Limitation Due to Turbulent Wall Boundary Layer by : Aerospace Corporation
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.
Book Synopsis Test Time in Low Pressure Shock Tubes by : Aerospace Corporation
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:
Book Synopsis Flow Nonuniformity in Shock Tubes Operating at Maximum Test Time by : H. Mirels
Download or read book Flow Nonuniformity in Shock Tubes Operating at Maximum Test Time written by H. Mirels and published by . This book was released on 1966 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: Shock tube flow nonuniformity is investigated in the limit where the shock and contact surface have reached their maximum separation. Ideal gases are considered. It is found that all fluid properties increase in value between the shock and contact surface. The nonuniformity is greatest when gamma (ratio of specific heats) is large and M sub s (shock Mach number) is low. For gamma = 5/3 and M sub s> or = 3, the static temperature, density, and pressure increase by about 8, 12 and 20%, respectively; the stagnation temperature increases by about 35%, and the stagnation pressure, dynamic pressure, and stagnation point heat transfer increase by about a factor of 2. These results apply to turbulent as well as laminar boundary layers. The variation of flow properties with distance behind the shock, as well as particle time of flight, is given for both wholly laminar and wholly turbulent wall boundary layers. These results are particularly important for chemical rate and heat transfer studies. (Author).
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Book Synopsis Gasdynamics of Explosions and Reactive Systems by : A. K. Oppenheim
Download or read book Gasdynamics of Explosions and Reactive Systems written by A. K. Oppenheim and published by Elsevier. This book was released on 2013-10-22 with total page 787 pages. Available in PDF, EPUB and Kindle. Book excerpt: Gas Dynamics of Explosions and Reactive Systems documents the proceedings of the 6th Colloquium held at the Royal Institute of Technology in Stockholm, Sweden, 22-26 August 1977. The meeting was held under the auspices of the Royal Swedish Academy of Sciences and the International Academy of Astronautics. The scientific program included over one hundred papers. The contributions in this volume are organized into four parts. Part I contains papers on gaseous detonations. It covers topics such as theoretical model of a detonation cell; spherical detonations in hydrocarbon-air mixtures; and shock wave propagation in tubes filled with water foams. Part II presents studies on explosions, such as the detonation of hydrogen azide and propagation of a laser-supported detonation wave. Part III examines condensed phase detonations. It includes papers on the mechanism of the divergent and convergent dark waves originating at the charge boundary in detonating liquid homogeneous explosives with unstable detonation front; and initiation studies in sensitized nitromethane. Part IV presents discussions on turbulent detonations, covering topics such as the computational aspects of turbulent combustion and problems and techniques in turbulent reactive systems.
Book Synopsis Technical Report - Jet Propulsion Laboratory, California Institute of Technology by : Jet Propulsion Laboratory (U.S.)
Download or read book Technical Report - Jet Propulsion Laboratory, California Institute of Technology written by Jet Propulsion Laboratory (U.S.) and published by . This book was released on 1965 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1974 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Advanced Hypersonic Test Facilities by : Frank K. Lu
Download or read book Advanced Hypersonic Test Facilities written by Frank K. Lu and published by AIAA. This book was released on 2002 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
Download or read book NASA Technical Paper written by and published by . This book was released on 1984 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis General Chemical Kinetics Computer Program for Static and Flow Reactions, with Application to Combustion and Shock-tube Kinetics by : David A. Bittker
Download or read book General Chemical Kinetics Computer Program for Static and Flow Reactions, with Application to Combustion and Shock-tube Kinetics written by David A. Bittker and published by . This book was released on 1972 with total page 216 pages. Available in PDF, EPUB and Kindle. Book excerpt: A general chemical kinetics program is described for complex, homogeneous ideal-gas reactions in any chemical system. Its main features are flexibility and convenience in treating many different reaction conditions. The program solves numerically the differential equations describing complex reaction in either a static system or one-dimensional inviscid flow. Applications include ignition and combustion, shock wave reactions, and general reactions in a flowing or static system. An implicit numerical solution method is used which works efficiently for the extreme conditions of a very slow or a very fast reaction. The theory is described, and the computer program and users' manual are included.
Book Synopsis High-Speed Flight Propulsion Systems by : S. N. B. Murthy
Download or read book High-Speed Flight Propulsion Systems written by S. N. B. Murthy and published by AIAA. This book was released on 1991 with total page 558 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis LSENS, a General Chemical Kinetics and Sensitivity Analysis Code for Homogeneous Gas-phase Reactions. 2: Code Description and Usage by : Krishnan Radhakrishnan
Download or read book LSENS, a General Chemical Kinetics and Sensitivity Analysis Code for Homogeneous Gas-phase Reactions. 2: Code Description and Usage written by Krishnan Radhakrishnan and published by . This book was released on 1994 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis of Test Times and Boundary Layer Induced Property Variations in a Circular Shock Tube by : John J. Bertin
Download or read book Analysis of Test Times and Boundary Layer Induced Property Variations in a Circular Shock Tube written by John J. Bertin and published by . This book was released on 1967 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Abstract Bulletin by : Defense Documentation Center (U.S.)
Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1964 with total page 1148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis J.P.L. Quarterly Technical Review by : Jet Propulsion Laboratory (U.S.)
Download or read book J.P.L. Quarterly Technical Review written by Jet Propulsion Laboratory (U.S.) and published by . This book was released on 1971-04 with total page 646 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Shock Tube Research by : J. L. Stollery
Download or read book Shock Tube Research written by J. L. Stollery and published by . This book was released on 1971 with total page 998 pages. Available in PDF, EPUB and Kindle. Book excerpt:
