Cylinder Shock Layer Density Profiles Measured in High Enthalpy Flows in HEG

Cylinder Shock Layer Density Profiles Measured in High Enthalpy Flows in HEG PDF Author: Klaus Hannemann
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Languages : en
Pages :

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Cylinder Shock Layer Density Profiles Measured in High Enthalpy Flows in HEG

Cylinder Shock Layer Density Profiles Measured in High Enthalpy Flows in HEG PDF Author: Klaus Hannemann
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ISBN:
Category :
Languages : en
Pages :

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New Results in Numerical and Experimental Fluid Mechanics IV

New Results in Numerical and Experimental Fluid Mechanics IV PDF Author: Christian Breitsamter
Publisher: Springer Science & Business Media
ISBN: 3540396047
Category : Technology & Engineering
Languages : en
Pages : 497

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This volume contains 59 papers presented at the 13th Symposium of STAB (German Aerospace Aerodynamics Association). In this association, all those German scientists and engineers from universities, research establishments and industry are involved who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics, mainly for aerospace but also in other applications. Many of the contributions give results from federal and European-Union sponsored projects. The volume gives a broad overview of the ongoing work in this field in Germany. Covered are flow problems of high and low aspect-ratio wings and bluff bodies, laminar flow control and transition, hypersonic flows, transition and fluid mechanical modelling, LES and DNS, numerical simulation, aeroelasticity, measuring techniques and propulsion flows.

Shock Waves

Shock Waves PDF Author: Klaus Hannemann
Publisher: Springer Science & Business Media
ISBN: 3540851682
Category : Science
Languages : en
Pages : 810

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The 26th International Symposium on Shock Waves in Göttingen, 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.

Shock Waves

Shock Waves PDF Author: Zonglin Jiang
Publisher: Springer Science & Business Media
ISBN: 3540270094
Category : Science
Languages : en
Pages : 1346

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The 24th International Symposium on Shock Waves (ISSW24) was held at the Beijing Friendship Hotel during July 11-16, 2004, in Beijing. It was a great pleasure for the Local Organizing Committee to organize the ISSW in China for the first time, because forty-seven years have passed since the First Shock Tube Symposium was held in 1957 at Albuquerque. The ISSW24 had to be postponed for one year because of the SARS outbreak in Beijing shortly before the Symposium was scheduled to be held in 2003, but it has achieved success due to the continuous support and kind understanding from all the delegates. It is very heart-warming to have had such an experience and I am very happy to have served as chairman for the Symposium. I would like to thank all for the contributions and help that they have given us over the past three years, without which we would not have had the Symposium. A total of 460 abstracts were submitted to the ISSW24. Each of the abstracts was evaluated by three members of the Scientific Review Committee and the decision on acceptance wasmade based on the reviewers' reports. 195oral papers,including 9plenary lectures, wereaccepted to be presented in three parallel sessions, and 135poster papers in three dedicated poster sessions. Topics discussed in these papers cover all aspects ofshock wave research.

30th International Symposium on Shock Waves 2

30th International Symposium on Shock Waves 2 PDF Author: Gabi Ben-Dor
Publisher: Springer
ISBN: 3319448668
Category : Technology & Engineering
Languages : en
Pages : 681

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Book Description
These proceedings collect the papers presented at the 30th International Symposium on Shock Waves (ISSW30), which was held in Tel-Aviv Israel from July 19 to July 24, 2015. The Symposium was organized by Ortra Ltd. The ISSW30 focused on the state of knowledge of the following areas: Nozzle Flow, Supersonic and Hypersonic Flows with Shocks, Supersonic Jets, Chemical Kinetics, Chemical Reacting Flows, Detonation, Combustion, Ignition, Shock Wave Reflection and Interaction, Shock Wave Interaction with Obstacles, Shock Wave Interaction with Porous Media, Shock Wave Interaction with Granular Media, Shock Wave Interaction with Dusty Media, Plasma, Magnetohyrdrodynamics, Re-entry to Earth Atmosphere, Shock Waves in Rarefied Gases, Shock Waves in Condensed Matter (Solids and Liquids), Shock Waves in Dense Gases, Shock Wave Focusing, Richtmyer-Meshkov Instability, Shock Boundary Layer Interaction, Multiphase Flow, Blast Waves, Facilities, Flow Visualization, and Numerical Methods. The two volumes serve as a reference for the participants of the ISSW30 and anyone interested in these fields.

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference: 02-2700 - 02-2926

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference: 02-2700 - 02-2926 PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 694

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41st AIAA Aerospace Sciences Meeting & Exhibit

41st AIAA Aerospace Sciences Meeting & Exhibit PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 594

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Shock-tube Heat-transfer Measurements on Inner Surface of a Cylinder (simulating a Flat Plate) for Stagnation-temperature Range 4,100 ̊to 8,300 ̊R

Shock-tube Heat-transfer Measurements on Inner Surface of a Cylinder (simulating a Flat Plate) for Stagnation-temperature Range 4,100 ̊to 8,300 ̊R PDF Author: Jim J. Jones
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 22

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892

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High Enthalpy Flows in the HEG Shock Tunnel

High Enthalpy Flows in the HEG Shock Tunnel PDF Author: Klaus Hannemann
Publisher:
ISBN:
Category :
Languages : en
Pages :

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