NDLI: Propagation characteristics of shock waves driven by gaseous detonation waves

Content Provider	Springer Nature Link
Author	Kato, S. Hashimoto, S. Uemichi, A. Kasahara, J. Matsuo, A.
Copyright Year	2010
Abstract	We experimentally investigated propagation characteristics of the shock wave driven by a gaseous detonation wave emerging from the open end of a cylindrical detonation tube. In the present study, we visualized the shock wave and exhaust flowfields using a shadowgraph optical system and we obtained peak overpressure in the tube axial direction and the continuous shape transformation of shock waves around the tube open end. We also obtained overpressure histories of the shock wave using piezo-pressure transducers within 201 m from the open end of the tube. We normalized and classified these results by four regions using non-dimensional pressure and distance which are independent of variety of mixture and tube diameter. In the vicinity of the open end of the tube, the shock wave is nearly planar and does not significantly attenuate, and the peak overpressure maintains approximately C–J pressure. Subsequently, the shock wave attenuates rapidly, transforming from quasi-spherical to spherical. Farther from the tube open end, the shock wave propagates with approximately sound characteristic so that the peak overpressure decreases proportional to 1/r. Eventually, the shock wave begins to attenuate more rapidly than ideal sound attenuation, which may be due to the viscous effect.
Starting Page	479
Ending Page	489
Page Count	11
File Format	PDF
ISSN	09381287
Journal	Shock Waves
Volume Number	20
Issue Number	6
e-ISSN	14322153
Language	English
Publisher	Springer-Verlag
Publisher Date	2010-09-18
Publisher Place	Berlin, Heidelberg
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Shock wave Detonation PDE Optical visualization SPL Condensed Matter Physics Acoustics Thermodynamics Engineering Fluid Dynamics Fluid- and Aerodynamics Engineering Thermodynamics, Heat and Mass Transfer
Content Type	Text
Resource Type	Article
Subject	Physics and Astronomy Mechanical Engineering

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

Rotary wave-ejector enhanced pulse detonation engine

Ionization in gaseous detonation waves

Wave propagation in gaseous small-scale channel flows

Comparative characteristics of strong shock and detonation waves in bubble media by an electrical wire explosion

On the influence of low initial pressure and detonation stochastic nature on Mach reflection of gaseous detonation waves

A chemical shock tube driven by detonation

Micro-blast waves using detonation transmission tubing

Effects of boundary layer on flame propagation generated by forced ignition behind an incident shock wave

Detonation wave initiated by explosive condensation of supersaturated carbon vapor

Propagation characteristics of shock waves driven by gaseous detonation waves

Similar Documents

Rotary wave-ejector enhanced pulse detonation engine

Ionization in gaseous detonation waves

Wave propagation in gaseous small-scale channel flows

Comparative characteristics of strong shock and detonation waves in bubble media by an electrical wire explosion

On the influence of low initial pressure and detonation stochastic nature on Mach reflection of gaseous detonation waves

A chemical shock tube driven by detonation

Micro-blast waves using detonation transmission tubing

Effects of boundary layer on flame propagation generated by forced ignition behind an incident shock wave

Detonation wave initiated by explosive condensation of supersaturated carbon vapor

Propagation characteristics of shock waves driven by gaseous detonation waves