Shock Tube Test Time Limitation Due to Turbulent Wall Boundary Layer

Shock Tube Test Time Limitation Due to Turbulent Wall Boundary Layer
Author: Aerospace Corporation
Publisher:
Total Pages: 72
Release: 1963
Genre: Boundary layer
ISBN:

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.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author:
Publisher:
Total Pages: 488
Release: 1995
Genre: Aeronautics
ISBN:

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.

Gasdynamics of Explosions and Reactive Systems

Gasdynamics of Explosions and Reactive Systems
Author: A. K. Oppenheim
Publisher: Elsevier
Total Pages: 787
Release: 2013-10-22
Genre: Science
ISBN: 1483150054

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.

Shock Tubes and Waves

Shock Tubes and Waves
Author: Charles E. Treanor
Publisher: SUNY Press
Total Pages: 1130
Release: 1982-01-01
Genre: Philosophy
ISBN: 9780873955959

Proceedings from a symposium on shock tubes and waves held July 6-9, 1981.

General Chemical Kinetics Computer Program for Static and Flow Reactions, with Application to Combustion and Shock-tube Kinetics

General Chemical Kinetics Computer Program for Static and Flow Reactions, with Application to Combustion and Shock-tube Kinetics
Author: David A. Bittker
Publisher:
Total Pages: 216
Release: 1972
Genre: Chemical kinetics
ISBN:

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.

High-Speed Flight Propulsion Systems

High-Speed Flight Propulsion Systems
Author: S. N. B. Murthy
Publisher: AIAA
Total Pages: 558
Release: 1991
Genre: Aerodynamics, Hypersonic
ISBN: 9781600863912

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.