- MODELLING AND EXPERIMENTAL INVESTIGATION OF REACTIVE SHEAR BANDS IN ENERGETIC SOLIDS LOADED IN TORSION
- Multiscale Computations of Fluid Flows Using an Adaptive Wavelet Method
- ANALYSIS FOR STEADY PROPAGATION OF A GENERIC RAM ACCELERATOR/OBLIQUE DETONATION WAVE ENGINE CONFIGURATION
- Calculation of Invariant Manifolds for Reacting Ashraf N. Al-Khateeb, Joseph M. Powers, Samuel Paolucci,
- Projective Space Method for Slow Invariant Manifolds of Reactive Systems
- Two-phase viscous modeling of compaction of granular materials Joseph M. Powersa)
- Diffusion Effects on Slow Invariant Manifolds Joshua D. Mengers
- CALCULATIONS FOR STEADY PROPAGATION OF A GENERIC RAM ACCELERATOR CONFIGURATION USING THE ROE METHOD
- AIAA JOURNAL Vol. 30, No. 11, November 1992
- AIAA JOURNAL Vol. 43, No. 5, May 2005
- Diffusion Correction to Slow Invariant Manifolds in a Short Length Scale Limit
- Spatial and Temporal Scales Coupling in Reactive Flows
- Shock Waves (2010) 20:445446 DOI 10.1007/s00193-010-0281-z
- Shock-Fitted Numerical Solutions for Two-Dimensional Detonations
- Modeling Gas Phase RDX Combustion with Intrinsic Low Dimensional Manifolds 1 Sandeep Singh2
- The AIAA Code Verification Project -Test cases for CFD Code Verification
- Standardized pseudospectral formulation of the inviscid supsersonic blunt body problem q
- Proceedings of IMECE2007 2007 ASME International Mechanical Engineering Congress and Exposition
- Advanced Multi-Scale Methods for Hypersonic J. M. Powers, D. Wirasaet and S. Paolucci
- Diffusion Effects on Slow Invariant Manifolds Joshua D. Mengers
- A KarhunenLoeve least-squares technique for optimization of geometry of a blunt body in supersonic flow q
- AIAA JOURNAL, VOL. 30, NO. 12: TECHNICAL NOTES 2985 2Peters, N., "Laminar Diffusion Flamelet Models in Non-Premixed
- Methodology and Analysis for Determination of Propagation Speed of High-Speed Propulsion Devices
- Shock Waves (1996) 6: 183-195 tCJ Springer Verlag 1996
- Combust. Sci. and Tech., 1998, Vol. 136, pp. 349-371 Reprints available directly from the publisher
- The Dynamics of Unsteady Detonation with Christopher M. Romick,
- Effects of Convection and Diffusion on Rational Reduction of Detailed Kinetic Schemes
- Uniqueness of chemical equilibria in ideal mixtures of ideal gases Joseph M. Powersa
- Introduction: Perspectives on Detonation-Based Propulsion DOI: 10.2514/1.26953
- Simulations of pulsating one-dimensional detonations with true fifth order accuracy q
- Mapped weighted essentially non-oscillatory schemes: Achieving optimal order near critical points q
- INSTITUTE OF PHYSICS PUBLISHING COMBUSTION THEORY AND MODELLING Combust. Theory Modelling 5 (2001) 163184 www.iop.org/Journals/ct PII: S1364-7830(01)13165-7
- Combust. Theory Modelling 3 (1999) 103122. Printed in the UK PII: S1364-7830(99)94093-7 Thermal explosion theory for shear localizing energetic solids
- Shock Waves (1996)6: 147-156 o Springer Verlag 1996
- JOURNAL OF PROPULSION AND POWER Vol. 11, No. I, January-February 1995
- JOURNAL OF PROPULSION AND POWER Vol. 10, No.4, July-Aug. 1994
- OBLIQUE DETONATIONS: THEORY AND PROPULSION APPLICATIONS
- AIAA JOURNAL Vol. 30, No.3, March 1992
- 280 COMBUSTION AND FLAME 80: 280-303 (1990) Theory of Two-Phase Detonation-Part II: Structure
- Reprinted from March 1989, Vol. Ill, Jouma! of Applied Mechanics J. M. Powers
- Application of the Slow Invariant Manifold Correction for Diffusion
- 49th AIAA Aerospace Science Meeting, 4-7 January 2011, Orlando, Florida The Dynamics of Unsteady Detonation with Diffusion
- Simulation of Compressible Reacting Flow using the Parallel Wavelet Adaptive Multiresolution
- Analysis of ReactionAdvectionDiffusion Spectrum of Laminar Premixed Flames
- A Two-Phase Micromorphic Model for Compressible Granular Materials
- Accurate Calculation of Detonation with an Adaptive Wavelet Method
- Verification, Validation, and Scientific Computing: Successes, Failures, and Challenges
- On the Relation Between Reaction Dynamics and Thermodynamics in Closed Systems
- 47th AIAA Aerospace Science Meeting, 5-8 January 2009, Orlando, Florida Calculation of Slow Invariant Manifolds for Reactive
- 47th AIAA Aerospace Science Meeting and Exhibit, 5-8 January 2009, Orlando, Florida The Dynamics of Unsteady Detonation in Ozone
- Solution of Reactive Compressible Flows Using an Adaptive Wavelet Method
- Computation of Slow Invariant Manifolds for Hydrogen-Air Systems
- 46th AIAA Aerospace Science Meeting and Exhibit, 7-10 January 2008, Reno, Nevada Shock-Fitted Calculation of Unsteady Detonation in
- On the Coupling Between Length and Time Scales in Reactive Flows
- The Thermodynamics of Slow Invariant Manifolds for Reactive Systems
- On the Computation of Approximate Slow Invariant Manifolds
- Mathematical Verification of Simulations of Reactive Flows with Embedded Discontinuities
- 43rd AIAA Aerospace Sciences Meeting and Exhibit, 10-13 January 2005, Reno, Nevada Exact Solutions for Two-Dimensional Reactive Flow
- 43rd AIAA Aerospace Sciences Meeting and Exhibit, 10-13 January 2005, Reno, Nevada Accurate Estimates of Fine Scale Reaction Zone
- 43rd AIAA Aerospace Sciences Meeting and Exhibit, 10-13 January 2005, Reno, Nevada Highly Accurate Numerical Simulations of Pulsating
- For permission to copy or to republish, contact the copyright owner named on the first page. For AIAA-held copyright, write to AIAA Permissions Department,
- On Computing Reactive Flows Using Slow S. Paolucci1
- NOVEL MODELING OF HYDROGEN/OXYGEN DETONATION Yevgenii Rastigejev
- Extended Abstract Model Formulation and Predictions
- Advanced Multi-Scale Methods for Hypersonic Z. J. Zikoski, C. M. Romick, J. M. Powers and
- One-dimensional slow invariant manifolds for spatially homogenous reactive systems
- Multidimensional Detonation Solutions from Reactive Navier-Stokes Equations 1
- Two-Phase Steady Detonation Analysis J. M. Powers, D. S. Stewart, and H. Krier
- Reaction zone structure for strong, weak overdriven, and weak underdriven oblique detonations
- JOURNAL OF PROPULSION AND POWER Vol. 22, No. 6, NovemberDecember 2006
- MODELING PYROTECHNIC SHOCK IN A NASA STANDARD INITIATOR DRIVEN PIN PULLER Keith A. Gonthier,
- 45th AIAA Aerospace Science Meeting and Exhibit, 8-11 January 2007, Reno, Nevada Verified Computations of Laminar Premixed Flames
- AIAA-2004-0655 Verification and Validation of
- AIAA JOURNAL Vol. 44, No. 2, February 2006
- THEORY OF DETONATION STRUCTURE FOR TWO-PHASE MATERIALS
- A Wavelet/ILDM Method for Computational Combustion 1 J. M. Powers2
- Reactive Flow Calculations with Intrinsic Low Dimensional Manifold Corrections for Convection and Diffusion 1 Sandeep Singh2
- 49th AIAA Aerospace Sciences Meeting, 4-7 Jan. 2011, Orlando, Florida Application of the Slow Invariant Manifold Correction
- Commun. Comput. Phys. doi: 10.4208/cicp.090709.021109a
- Computation of compaction in compressible granular material Michael T. Cochran a,1
- Advanced Multi-Scale Methods for Hypersonic Z. J. Zikoski, C. M. Romick, J. M. Powers and
- A NUMERICAL INVESTIGATION OF SELF-PROPAGATING TWO-PHASE DETONATION Paper Number 105
- 48th AIAA Aerospace Science Meeting, 4-7 January 2010, Orlando, Florida Analysis of the Reaction-Advection-Diffusion
- Journal of Computational Physics 163, 376433 (2000) doi:10.1006/jcph.2000.6569, available online at http://www.idealibrary.com on
- Joseph M. Powers e-mail: powers@nd.edu
- Advances and Applications of Intrinsic Low Dimensional Manifold Theory Joseph M. Powers, Samuel Paolucci, and Sandeep Singh
- COMBUSTION AND FLAME 80:264-279 (1990) Theory of Two-Phase Detonation-Part I: Modeling
- Simulation of Multidimensional Detonations in an H2-O2-Ar Mixture Using an Adaptive
- Journal of Hazardous Materials, 13 (1986) 121-133 Elsevier Science Publishers B.V., Amsterdam -Printed in The Netherlands
- 44th AIAA Aerospace Sciences Meeting and Exhibit, 9-12 January 2006, Reno, Nevada Accurate Estimates of Fine Scale Reaction Zone
- REACTION ZONE STRUCTURE OF WEAK UNDERDRIVEN OBLIQUE DETONATIONS
- The Dynamics of Unsteady Detonation with Christopher M. Romick,
- On slow manifolds of chemically reactive systems Sandeep Singh,a)
- Slow Invariant Manifolds for Reactive-Diffusive Systems
- Verification and validation of detonation simulation: topical review
- Verified Calculation of Multiscale Combustion in Gaseous Mixtures
- The Dynamics of Detonation with WENO and Navier-Stokes Shock-Capturing
- 50th AIAA Aerospace Sciences Meeting, 9-12 Jan. 2012, Nashville, Tennessee Model Reduction for Reaction-Diffusion Systems
- Dynamics of Unsteady Inviscid and Viscous Detonations in Hydrogen-Air
- Verified Calculation of Multiscale Combustion in Gaseous Mixtures
- AIAA Aerospace Sciences Meeting and Exhibit, 9-12 January 2012, Nashville, Tennessee. Dynamics of Unsteady Inviscid and Viscous
- Slow Invariant Manifolds for Reaction-Diffusion Systems
