๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Shock Waves || Numerical studies of shock vector control for deflecting nozzle exhaust flows

โœ Scribed by Hannemann, Klaus; Seiler, Friedrich


Book ID
121653098
Publisher
Springer Berlin Heidelberg
Year
2009
Tongue
English
Weight
315 KB
Edition
1
Category
Article
ISBN
354085181X

No coin nor oath required. For personal study only.

โœฆ Synopsis


The 26th International Symposium on Shock Waves in Gรถttingen, Germany was jointly organised by the German Aerospace Centre DLR and the French-German Research Institute of Saint Louis ISL. The year 2007 marked the 50th anniversary of the Symposium, which first took place in 1957 in Boston and has since become an internationally acclaimed series of meetings for the wider Shock Wave Community. The ISSW26 focused on the following areas: Shock Propagation and Reflection, Detonation and Combustion, Hypersonic Flow, Shock Boundary Layer Interaction, Numerical Methods, Medical, Biological and Industrial Applications, Richtmyer Meshkov Instability, Blast Waves, Chemically Reacting Flows, Diagnostics, Facilities, Flow Visualisation, Ignition, Impact and Compaction, Multiphase Flow, Nozzles Flows, Plasmas and Propulsion. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 26 and individuals interested in these fields.


๐Ÿ“œ SIMILAR VOLUMES


Study of initial shock wave in exhausted
โœ Qiang Xu; Jun Li ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 207 KB

The initial show wave is a non-stationary phenomenon in the initial stage of an exhausted ยฏow ยฎeld. Its movement characteristic and development process cannot be mastered accurately with the use of contact-type measurement methods, such as pressure and velocity measurements. An experimental study of