Shock-Fitted Calculations of Unsteady Detonation in Ozone
Author:
Affiliation:
1. Los Alamos National Laboratory
2. University of Notre Dame
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1036
Reference21 articles.
1. Simulations of pulsating one-dimensional detonations with true fifth order accuracy
2. Mapped weighted essentially non-oscillatory schemes: Achieving optimal order near critical points
3. Accurate Spatial Resolution Estimates for Reactive Supersonic Flow with Detailed Chemistry
4. Viscous detonation in H2‒O2‒Ar using intrinsic low-dimensional manifolds and wavelet adaptive multilevel representation
5. Resolving the shock-induced combustion by an adaptive mesh redistribution method
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. An Approximate Chemical Kinetics Method for Detonation Products;Physics Procedia;2015
2. Numerical simulation of changes in the composition of detonation products of a free volume of a combustible mixture;Combustion, Explosion, and Shock Waves;2012-05
3. The Dynamics of Unsteady Detonation in Ozone;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
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