Papers – Paul Cizmas

1985

1. ”Application of Symbolic Logic to the Morphometric Study of Coronary Diabetic Microangiopathy,” The First International Symposium for Science on Form, Tsukuba, Japan, 1985 by I. Basca, C. Vasilescu and P. Cizmas.

1987

1. ”Velocity Distribution on Autovehicle Contour Through Numerical Simulation,” Bul. Inst. Politeh. Ser. Transp. Aeronave, 49, 43–50 (1987) by M. Oprean, P. Cizmas and F. Stoenescu.
2. ”Computation Through Numerical Simulation of Vehicle Aerodynamic Characteristics,” Proceedings of ISATA, Vol. II, No. 87183, Munich, West Germany, 1987 by P. Cizmas, P. Jebelean, M. Oprean and F. Stoenescu.

1989

1. ”Expert System for the Aerodynamical Study of Car Shape,” Proceedings of the International Conference OPTI-89, Southampton, U.K., 1989 by P. Cizmas, P. Jebelean, M. Oprean and D. Serban.

1990

1. ”Conformal Mapping Extension of Cascade Plates to Cascade Airfoils of a Given Shape,” Journal of the Romanian Academy, Studii si Cercetari de Mecanica Aplicata, 49(5-6), 467–476 (1990) by C. Berbente and P. Cizmas.
2. ”Axial Symmetrically Loaded Discs and Plates Calculated by the Three Unknowns Method,” Journal of the Romanian Academy, Studii si Cercetari de Mecanica Aplicata, 49(1), 71–84 (1990) by P. Cizmas.

1991

1. ”Disc Shape Optimization Using the Three Unknowns Method,”
  Proceedings of the International Conference OPTI-91, Boston, MA, June
  1991 by P. Cizmas.

1995

1. ”Computation of Steady and Unsteady Viscous Flows Using a Simultaneously Coupled Inviscid-Viscous InteractionTechnique,” Journal of Fluid and Structures, 9, 639–657 (1995) by
  P. Cizmas and K. C. Hall.
2. ”A Viscous-Inviscid Model of
  Unsteady Small Disturbance Flows in Cascades,” Paper AIAA 95-2655,
  31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San
  Diego, CA, July 10-13, 1995 by P. Cizmas and K. C. Hall.
3. ”Simultaneous Method to Calculate
  Interacting Boundary Layers Using a Solid Body Model,” AIAA Paper
  95-2154, 26th AIAA Fluid Conference, San Diego, CA, June 19-22, 1995 by
  P. Cizmas.

1996

1. ”Flow About a Slotted
  Cylinder-Airfoil Configuration in a Wind Tunnel,” Journal of
  Aircraft, 33, 716–721 (1996) by P. Cizmas, D. M. Tang and E. H. Dowell.
2. ”Experiments and Analysis of
  Gust Generator in a Wind Tunnel,” Journal of Aircraft, 33, 139–148
  (1996) by D. M. Tang, P. Cizmas and E. H. Dowell.
3. ”Reduced-Order Modeling of
  Unsteady Viscous Flow in a Compressor Cascade,” AIAA Paper 96-2572,
  32th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 1-3, 1996, Lake
  Buena Vista, FL by R. Florea, K. C. Hall and P. G. A. Cizmas.
4. ”Aerodynamics of a Rotating Slotted Cylinder and its Applications,”
  Third International Colloquium on Bluff Body Aerodynamics and
  Applications, Blacksburg, VA, July 28-August 1, 1996 by D. M. Tang,
  P. Cizmas and E. H. Dowell.

1997

1. ”Eigenmode Analysis of
  Unsteady Viscous Flows in Turbomachinery Cascades,” The Eighth
  International Symposium on Unsteady Aerodynamics and Aeroelasticity of
  Turbomachines, Stockholm, Sweden, September 14-18, 1997 by R. Florea,
  K. C. Hall and P. Cizmas.
2. ”Parallel Computation of
  Rotor-Stator Interaction,” The Eighth International Symposium on
  Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Stockholm,
  Sweden, September 14-18, 1997 by P. Cizmas and R. Subramanya.

1998

1. ”Reduced-Order Modeling of Unsteady
  Viscous Flow in a Compressor Cascade,” AIAA Journal, 36, 1039–1048
  (1998) by R. Florea, K. C. Hall and P. G. A. Cizmas.
2. ”Parallel Computation of
  Turbine Blade Clocking,” Paper AIAA 98-3598, 34th AIAA/ASME/SAE/ASEE
  Joint Propulsion Conference, Cleveland, Ohio, July 13-15, 1998 by
  P. Cizmas and D. J. Dorney.

1999

1. ”Parallel Computation of
  Turbine Blade Clocking,” International Journal of Turbo &
  Jet-Engines, 16, 49–60 (1999) by P. Cizmas and D. J. Dorney.
2. ”The Influence of Clocking on
  Unsteady Forces of Compressor and Turbine Blades,” The Fourteenth
  International Symposium on Airbreathing Engines, Florence, Italy,
  September 1999 by P. G. A. Cizmas and D. J. Dorney.
3. ”Full-Annulus Simulations of Airfoil
  Clocking in a 1-1/2 Stage Axial Compressor,” ASME Paper 99-GT-023,
  International Gas Turbine and Aeroengine Conference, Indianapolis,
  Indiana, June 1999 by D. J. Dorney, D. L. Sondak, P. G. A. Cizmas,
  V. E. Saren and N. M. Savin.
4. ”Full-Annulus Simulations of Airfoil
  Clocking in a Compressor at Off-Design Operating Conditions,” AIAA
  Paper 99-2383, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and
  Exhibit, Los Angeles, June 1999 by D. J. Dorney, D. L. Sondak,
  P. G. A. Cizmas, V. E. Saren and N. M. Savin.
5. ”Effects of Hot Streak/Airfoil Ratios in
  a High-Subsonic Single-Stage Turbine,” AIAA Paper 99-2384, 35th
  AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles,
  Jun. 1999 by D. J. Dorney, D. L. Sondak and P. G. A. Cizmas.

2000

1. ”Full-Annulus Simulations of Airfoil Clocking in a Compressor at
  Off-Design Operating Conditions,” International Journal of Turbo
  & Jet-Engines, 17, 95–117 (2000) by D. J. Dorney, S. L. Sondak,
  P. G. A. Cizmas, V. E. Saren and N. M. Savin.
2. ”The Influence of Clocking on
  Unsteady Forces of Compressor and Turbine Blades,” International
  Journal of Turbo & Jet-Engines, 17, 133–142 (2000) by P. G. A. Cizmas and
  D. J. Dorney.
3. ”Effects of Hot Streak/Airfoil Ratios in a High-Subsonic Single-Stage
  Turbine,” International Journal of Turbo and Jet Engines,
  17, 119–132 (2000) by D. J. Dorney, D. L. Sondak and P. G. A.
  Cizmas.
4. ”LES Calibration of a Turbulent
  Potential Model for Turbomachinery Flows,” AIAA Paper 2000-3203, 36th
  AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, Alabama, July
  2000 by S. M. Mitran and P. G. A. Cizmas.
5. ”Influence of Inter-Row
  Gap Value on Turbine Losses,” The Eight International Symposium on
  Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-8),
  Honolulu, Hawaii by P. G. A. Cizmas, C. R. Hoenninger, S. Chen and
  H. F. Martin.

2001

1. ”Optimal Placement of Cooling Flow
  Tubes in a Wall Heated from the Side,” International Journal of
  Transport Phenomena, 3, pp. 331-343 (2001) by P. G. A. Cizmas and
  A. Bejan.
2. ”A Parallel Algorithm for
  Simulation of Unsteady Flows in Multistage Turbomachinery,”
  International Journal of Turbo and Jet Engines, 18, 117–131 (2001) by
  P. G. A. Cizmas and R. Subramanya.
3. ”Influence of Inter-Row
  Gap Value on Turbine Losses,” International Journal of Rotating
  Machinery, 7, 335–349 (2001) by P. G. A. Cizmas, C. R. Hoenninger,
  S. Chen and H. F. Martin.
4. ”A 3-D Hybrid Mesh Generation for
  Turbomachinery Cascades,” AIAA Paper 2001-3209, 37th
  AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Salt Lake City, Utah, 8-11
  July 2001 by K. S. Kim and P. G. A. Cizmas.
5. ”The Influence of Blade-forced
  Vibration on Turbine Rotor-Stator Interaction,” AIAA Paper 2001-3472,
  37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Salt Lake City, Utah,
  8-11 July 2001 by J. Collard and P. G. A. Cizmas.
6. ”A CFD Method for Axial Thrust Load
  Prediction of Centrifugal Compressors,” ASME Paper 2001-GT-0568, 46th
  ASME International Gas Turbine Congress, New Orleans, Louisiana, June 4-7,
  2001 by Z. Han and P. G. A. Cizmas.

2002

1. ”A 3-D Hybrid Mesh Generation
  for Turbomachinery Cascades,” AIAA Journal of Propulsion and Power,
  18, 536–543 (2002) by K. S. Kim and P. G. A. Cizmas.
2. ”Numerical Simulation of
  Combustion and Rotor-Stator Interaction in a Turbine-Combustor,” The
  Ninth International Symposium on Transport Phenomena and Dynamics of
  Rotating Machinery (ISROMAC-9), Honolulu, Hawaii, February 10-14, 2002 by
  D. D. Isvoranu and P. G. A. Cizmas.

2003

1. ”Numerical Simulation of
  Combustion and Rotor-Stator Interaction in a Turbine-Combustor,”
  International Journal of Rotating Machinery, 9, 363–374 (2003) by
  D. D. Isvoranu and P. G. A. Cizmas.
2. ”The Accurate Element Method:
  A new paradigm for numerical solution of ordinary differential
  equations,” Proceedings of the Romanian Academy, Series A, 3, 1–7
  (2003) by M. Blumenfeld and P. Cizmas (communicated by Academician
  R. Voinea).
3. ”Proper Orthogonal Decomposition
  of Spatio-Temporal Patterns in Fluidized Beds,” Chemical Engineering
  Science, 58, 4417–4427 (2003) by P. G. A. Cizmas, A. Palacios, T. O’Brien
  and M. Syamlal.
4. ”The Effects of Vibrating
  Blades on Turbomachinery Rotor-Stator Interaction,” International
  Journal of Turbo & Jet-Engines, 20, 17–39 (2003) by J. Collard and
  P. G. A. Cizmas.
5. ”Proper Orthogonal Decomposition
  of Turbine Rotor-Stator Interaction,” AIAA Journal of Propulsion and
  Power, 19, 268–281 (2003) by P. G. A. Cizmas and A. Palacios.
6. ”A CFD Method for Axial Thrust
  Load Prediction of Centrifugal Compressors,” International Journal of
  Turbo & Jet-Engines, 20, 1–16 (2003) by Z. Han and P. G. A. Cizmas.
7. ”The Accurate Element
  Method: A Novel Method for Integrating Ordinary Differential
  Equations,” Advances in the Astronautical Sciences, 115, 446–461
  (2003) by M. Blumenfeld and P. Cizmas.
8. ”Analysis of Unsteady
  Aerodynamics Effects in a Turbine-Combustor,” 10th International
  Symposium on Unsteady Aerodynamics, Aeroacoustics, & Aeroelasticity of
  Turbomachines, Durham, North Carolina, 7-11 September, 2003 by
  P. G. A. Cizmas, H. Flitan, T. Lippert, D. Bachovchin and D. Little.
9. ”A Novel Method for Integrating Ordinary Differential Equations,”
  John Junkins Astrodynamics Symposium, College Station, Texas,
  23-24 May, 2003 by P. G. A. Cizmas and M. Blumenfeld.
10. ”Numerical Prediction of
  Unsteady Blade Loading in a Turbine-Combustor,” 8th National Turbine
  Engine High Cycle Fatigue Conference, Monterey, California, 14-16 April,
  2003 by P. G. A. Cizmas, H. Flitan and D. D. Isvoranu.

2004

1. ”Experimental Analysis and
  Visualization of Spatio-Temporal Bubble Patterns in Spouted Fluidized
  Beds,” Chaos, 14, 499–509 (2004) by A. Palacios, C. Finney,
  P. G. A. Cizmas, S. Daw and T. O’Brien.
2. ”Numerical and Experimental Investigation of In Situ Reheat,”
  Turbine Engine Technology Symposium, Dayton, OH, 30 August – 2 September,
  2004 by P. G. A. Cizmas and T. Lippert.
3. ”The influence of in situ
  reheat on turbine-combustor performance,” ASME Paper 2004-GT-54071,
  49th ASME International Gas Turbine Congress, Vienna, Austria, 14-17 June,
  2004 by S. Chambers, H. Flitan, P. G. A. Cizmas, T. Lippert, D.
  Bachovchin and D. Little.
4. ”Eigenvalues of Trusses
  and Beams Using the Accurate Element Method,” 2004 International ANSYS
  Conference, Pittsburgh, PA, 24-26 May, 2004 by M. Blumenfeld and
  P. Cizmas.

2005

1. ”A Reduced Order Model for a Bubbling
  Fluidized Bed based on Proper Orthogonal Decomposition,” Computers
  and Chemical Engineering, 30, 243–259 (2005) by T. Yuan, P. G. Cizmas and
  T. O’Brien.
2. ”Aeroelastic Analysis for Future
  Air Vehicle Concepts Using a Fully Nonlinear Methodology,” AIAA Paper
  2005-2171, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and
  Materials Conference, Austin, Texas, 18-21 April, 2005 by T. W. Strganac,
  P. G. Cizmas, C. Nichkawde, J. Gargoloff and P. Beran.

2006

1. ”The Influence of In Situ Reheat
  on Turbine-Combustor Performance,” ASME Journal of Engineering for
  Gas Turbines and Power, 128, 560–572 (2006) by S. B. Chambers, H. Flitan,
  P. Cizmas, D. Bachovchin, T. Lippert and D. Little.
2. ”Parallel Algorithm for Fully
  Nonlinear Aeroelastic Analysis,” AIAA Paper 2006-2073, 47th
  AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials
  Conference, Newport, RI, May, 2006 by J. Gargoloff, P. G. Cizmas,
  T. W. Strganac and P. Beran.
3. ”Dimensionless Parameters for Modeling Sand Particle Erosion of
  Polyurethane Coatings,” 9th Joint FAA/DOD/NASA Conference on Aging
  Aircraft, Atlanta, Georgia, March 2006 by J. C. Slattery and
  P. G. A. Cizmas.

2007

1. ”Dimensionless Correlation for
  Sand Erosion of Families of Polymers,” Wear, 262, 316–319 (2007) by
  P. G. Cizmas and J. C. Slattery.
2. ”A Numerical Method for
  Nonlinear Aeroelastic Analysis of Wings with Large Deformation,”
  International Forum on Aeroelasticity and Structural Dynamics, Stockholm,
  Sweden, June, 2007 by P. G. A. Cizmas, J. I. Gargoloff, T. W. Strganac
  and P. S. Beran.
3. ”An Acceleration Approach for
  Reduced-Order Models Based on Proper Orthogonal Decomposition,” AIAA
  Paper 2007-713, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno,
  Nevada, January, 2007 by P. G. A. Cizmas.
4. ”Mesh Generation and
  Deformation Algorithm for Aeroelasticity Simulations,” AIAA Paper
  2007-556, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada,
  January, 2007 by J. I. Gargoloff and P. G. A. Cizmas.
5. ”A Parallel Multigrid
  Algorithm for Aeroelasticity Simulations,” AIAA Paper 2007-330, 45th AIAA
  Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January, 2007 by
  J. I. Gargoloff, P. G. A. Cizmas, T. W. Strganac and P. S. Beran.
6. ”Numerical and Experimental
  Investigation of a Serpentine Inlet Duct,” AIAA Paper 2007-842, 45th
  AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January, 2007
  by A. M. Kirk, A. Kumar, J. I. Gargoloff, O. K. Rediniotis and
  P. G. A. Cizmas.

2008

1. ”Acceleration Techniques for
  Reduced-Order Models Based on Proper Orthogonal Decomposition,”
  Journal of Computational Physics, 227, 7791–7812 (2008) by
  P. G. A. Cizmas, B. R. Richardson, T. A. Brenner, T. J. O’Brien and
  R. W. Breault.
2. ”Mesh Generation and
  Deformation Algorithm for Aeroelasticity Simulations,” Journal of
  Aircraft, 45, 1062–1066 (2008) by P. G. A. Cizmas and J. I. Gargoloff.
3. ”Reduction of Jet Engine
  Thermal Signature,” International Journal of Turbo and Jet Engines,
  25, 1–12 (2008) by J. Guarnieri and P. G. Cizmas.
4. ”Single-Stage Axial
  Compressor for the Study of Rotating Stall Suppression,” AIAA Paper
  2008-4994, 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Hartford,
  CT, 21-23 July 2008 by F. Carpenter, S. Johnson, P. G. A. Cizmas and
  O. Rediniotis.
5. ”An Assessment of a Proper
  Orthogonal Decomposition Reduced-Order Model for Nonlinear
  Aeroelasticity,” NATO RTO Specialists’ Meeting AVT-154 Advanced Methods
  in Aeroelasticity, Loen, Norway, Oct. 2008 by P. G. A. Cizmas and
  P. Beran.

2009

1. ”Recent Developments in Numerical
  Simulation of Nonlinear Aeroelastic Phenomena” Acta Technica
  Napocensis – Series: Applied Mathematics and Mechanics, 52, Vol. II,
  13–18 (2009) by P. G. A. Cizmas.
2. ”Numerical
  and Experimental Investigation of a Serpentine Inlet Duct,”
  International Journal of Computational Fluid Dynamics, 23, 245–258 (2009)
  by A. M. Kirk, J. I. Gargoloff, O. K. Rediniotis and P. G. A. Cizmas.
3. ”A High-Fidelity
  Nonlinear Aeroelastic Model for Aircraft with Large Wing
  Deformation,” International Forum on Aeroelasticity and Structural
  Dynamics, Seattle, WA, June 2009 by P. G. A. Cizmas, B. A. Freno,
  T. A. Brenner and G. D. Worley.
4. ”Aeroelastic Analysis of a
  Transonic Wing for Design of Local Nonlinear Attachments,” AIAA Paper
  2009-2365, 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics,
  and Materials Conference, Palm Springs, CA, May 2009 by D. M. McFarland,
  P. Cizmas, T. Strganac, L. Bergman, Y. Lee, A. Vakakis and S. Hubbard.
5. ”Internal Plenum
  Design and Testing for an Oscillatory Blowing Stall Suppression
  System,” AIAA Paper 2009-1242, 47th AIAA Aerospace Sciences Meeting,
  Orlando, FL, Jan. 2009 by F. Carpenter, S. Johnson, P. G. A. Cizmas and
  O. Rediniotis.
6. ”Prediction of Fluid
  Instabilities in Hole-Pattern Stator Seals,” AIAA Paper 2009-786,
  47th AIAA Aerospace Sciences Meeting, Orlando, FL, Jan. 2009 by
  D. Liliedahl and P. G. A. Cizmas.
7. ”Practical Aspects
  of the Implementation of Proper Orthogonal Decomposition,” AIAA Paper
  2009-918, 47th AIAA Aerospace Sciences Meeting, Orlando, FL, Jan. 2009 by
  T. Brenner, P. G. A. Cizmas, T. O’Brien and R. Breault.

2010

1. ”Augmented Proper Orthogonal
  Decomposition for Problems with Moving Discontinuities,” Powder
  Technology, 203, 78–85 (2010) by T. A. Brenner, R. L. Fontenot,
  P. G. A. Cizmas, T. J. O’Brien and R. W. Breault.
2. ”A Parallel
  Multigrid Algorithm for Aeroelasticity Simulations,” Journal of
  Aircraft, 47, 53–63 (2010) by P. G. A. Cizmas, J. I. Gargoloff,
  T. W. Strganac and P. S. Beran.
3. ”Prediction of
  Aeroacoustic Resonance in Cavities of Hole-Pattern Stator Seals,”
  GT2010-23218, ASME Turbo Expo 2010: Power, Sea and Air, Glasgow, UK, June
  2010 by D. N. Liliedahl, F. L. Carpenter and P. G. A. Cizmas.
4. ”Turbomachinery Aeroelastic Analysis Using Proper Orthogonal
  Decomposition Method,” Propulsion – Safety and Affordable
  Readiness Conference, Jacksonville, FL, March 2010 by P. G. A.
  Cizmas.

2011

1. ”A Coordinate Transformation for
  Unsteady Boundary Layer Equations,” INCAS Bulletin, 3, Issue 4,
  35–45 (2011) by P. G. A. Cizmas.
2. ”Role of Differential Entropy
  Inequality in Chemically Reacting Flows,” Chemical Engineering
  Science, 66, 5236–5243 (2011) by J. C. Slattery, P. G. A. Cizmas,
  A. N. Karpetis and S. B. Chambers.
3. ”A Computationally
  Efficient Non-Linear Beam Model,” International Journal of Non-Linear
  Mechanics, 46, 854–869, (2011) by B. A. Freno and P. G. A. Cizmas.
4. ”Prediction of
  Aeroacoustic Resonance in Cavities of Hole-Pattern Stator Seals,”
  Journal of Engineering for Gas Turbines and Power – Transactions of the
  ASME, 133(2), 022504 (2011) by D. N. Liliedahl, F. L. Carpenter and
  P. G. A. Cizmas.
5. ”Stability Enhancement of a
  Transonic Wing Using a Simple Passive Attachment,” AIAA Atmospheric
  Flight Mechanics Conference, Portland, Oregon, Aug. 8-11, 2011 by
  S. Hubbard, D. M. McFarland, A. F. Vakakis, L. A. Bergman, R. L.
  Fontenot, R. L. Brown, P. G. A. Cizmas and T. W. Strganac.
6. ”Assessment of the Numerical
  Modeling of a Transonic Wing Aeroelastic Response,” International
  Forum on Aeroelasticity and Structural Dynamics, Paris, France, June 2011
  by R. L. Fontenot, S. Hubbard, R. L. Brown, D. M. McFarland, P. G. A.
  Cizmas, A. Vakakis and L. Bergman.
7. ”A Reduced-Order Model of the Reynolds-averaged Navier-Stokes
  Equations Based on the Proper Orthogonal Method,” Propulsion –
  Safety and Affordable Readiness Conference, Jacksonville, FL, March
  2011 by T. Brenner and P. G. A. Cizmas.
8. ”The Role of Structural
  Nonlinearities in Wind Turbine Blade Aeroelastic Analysis,” AIAA
  Paper 2011-995, 49th AIAA Aerospace Sciences Meeting including the New
  Horizons Forum and Aerospace Exposition, Orlando, Florida, Jan. 4-7, 2011
  by B. A. Freno, R. L. Brown and P. G. A. Cizmas.

2012

1. ”A
  Reduced-Order Model for Heat Transfer in Multiphase Flow and Practical
  Aspects of the Proper Orthogonal Decomposition,” Computers and
  Chemical Engineering, 43, pp. 68–80 (2012) by T. A. Brenner, and
  R. L. Fontenot, P. G. A. Cizmas, T. J. O’Brien and R. W. Breault.
2. ”An Investigation into the
  Significance of the Non-Linear Terms in the Equations of Motion for a
  Cantilevered Beam,” International Journal of Non-Linear Mechanics,
  47, 84–95 (2012) by B. A. Freno and P. G. A. Cizmas.
3. ”Aeroelastic Simulation
  of Structures in Hypersonic Flow,” 53rd Structures, Structural
  Dynamics, and Materials Conference, Honolulu, Hawaii, April 23-26, 2012 by
  R. L. Brown, K. Das, P. G. A. Cizmas and J. Whitcomb.
4. ”Proper Orthogonal
  Decomposition Applied to the Reynolds-Averaged Navier–Stokes
  Equations,” 50th AIAA Aerospace Sciences Meeting including the New
  Horizons Forum and Aerospace Exposition, AIAA-2012-314, Nashville,
  Tennessee, Jan. 9-12, 2012 by B. A. Freno, T. A. Brenner and P. G. A.
  Cizmas.

2013

1. ”Using Proper Orthogonal
  Decomposition to Model Off-reference Flow Conditions,” International
  Journal of Non-Linear Mechanics, 54, 76–84 (2013) by B. A. Freno,
  T. A. Brenner and P. G. A. Cizmas.
2. ”A Reduced-Order Model for
  Turbomachinery Flows using Proper Orthogonal Decomposition,”
  Proceedings of the ASME Turbo Expo 2013, SanAntonio, Texas, June 3-7, 2013
  by T. A. Brenner, F. L. Carpenter, B. A. Freno and P. G. A. Cizmas.
3. ”A Proper Orthogonal
  Decomposition Method for Nonlinear Flows with Deforming Meshes,” 51st
  AIAA Aerospace Sciences Meeting, Grapevine, Texas, January 7-10, 2013 by
  B. A. Freno and P. G. A. Cizmas.

2014

1. ”A Proper Orthogonal
  Decomposition Method for Nonlinear Flows with Deforming Meshes,”
  International Journal of Heat and Fluid Flow, 50, 145–159 (2014) by
  B. A. Freno and P. G. A. Cizmas.
2. ”Transonic
  Aeroelastic Instability Suppression for a Swept Wing by Targeted Energy
  Transfer,” Journal of Aircraft, 51, 1467–1482 (2014) by
  S. A. Hubbard, R. L. Fontenot, D. M. McFarland, P. G. A. Cizmas,
  L. A. Bergman, T. W. Strganac and A. F. Vakakis.
3. ”A Numerical Investigation of
  Actively Cooled Structures in Hypersonic Flow,” Journal of Aircraft,
  51, 1522–1531 (2014) by R. L. Brown, K. Das, P. G. A. Cizmas and
  J. D. Whitcomb.
4. ”Modeling of Unsteady Flows Using Reduced-Order Models Based on the
  Proper Orthogonal Decomposition,” International Conference of Aerospace
  Sciences ”AEROSPATIAL 2014”, Bucharest, Romania (2014) by T. A. Brenner,
  F. L. Carpenter, B. A. Freno, R. L. Fontenot and P. G. A. Cizmas.
5. ”Creating Reduced Kinetics
  Models that Satisfy the Entropy Inequality,” ASME Turbo Expo 2014,
  GT2014-25694, Dusseldorf, Germany (2014) by N. H. Jones, P. G. A. Cizmas
  and J. C. Slattery.
6. ”The Use of Dynamic Basis
  Functions in Proper Orthogonal Decomposition,” SciTech 2014,
  AIAA-2014-1436, National Harbor, Maryland (2014) by B. A. Freno,
  N. R. Matula, R. L. Fontenot and P. G. A. Cizmas.

2015

1. ”Creating Reduced
  Kinetics Models that Satisfy the Entropy Inequality,” Journal of
  Engineering for Gas Turbines and Power – Transactions of the ASME, 137,
  071504-1–9 (2015) by N. H. Jones, P. G. A. Cizmas and J. C. Slattery.
2. ”The Use of Dynamic Basis
  Functions in Proper Orthogonal Decomposition,” Journal of Fluids and
  Structures, 54, 332–360 (2015) by B. A. Freno, N. R. Matula,
  R. L. Fontenot and P. G. A. Cizmas.
3. ”Numerical Investigation of the Effects of Swirl Brake Design on
  Labyrinth Seal Leakage Flow,” Society of Engineering Science,
  College Station, Texas (2015) by N. R. Matula and P. G. A. Cizmas.

2016

1. ”Macro-Scale Fracture
  Analysis of Isothermal Composites: Theory and Seven Applications,”
  Engineering Fracture Mechanics, 163, 366–380 (2016) by J. C. Slattery and
  P. G. A. Cizmas.
2. ”A Reduced-Order Model for Turbomachinery Aeroelastic Analysis Based
  on the Zeta-Coordinate,” Propulsion Safety and Sustainment Conference,
  Grapevine, Texas (2016) by P. G. A. Cizmas.

2017

1. ”Experimental Validation of a
  Pulse Modulated Flow Control Actuator for Turbomachinery,” Journal of
  Propulsion and Power, 33, 1358–1368 (2017) by S. Johnson,
  F. L. Carpenter, O. K. Rediniotis and P. G. A. Cizmas.
2. ”Constrained reduced-order models
  based on proper orthogonal decomposition,” Comput. Methods
  Appl. Mech. Engrg., 321, 18–34 (2017) by S. R. Reddy, B. A. Freno,
  P. G. A. Cizmas, S. Gokaltun, D. McDaniel, G. S. Dulikravich.
3. ”Reduced-Order Methane-Air Combustion Mechanisms that Satisfies the
  Differential Entropy Inequality,” Constructal Law & Second Law
  Conference 2017, 568–591, Bucharest, Romania, May 15–16 (2017) by
  A. E. Ream, J. C. Slattery and P. G. A. Cizmas.
4. ”Transonic Fan Performance
  Evaluated with Different Solution Limiters,” Proceedings of the ASME
  Turbo Expo 2017, Charlotte, North Carolina by F. L. Carpenter and
  P. G. A. Cizmas.
5. ”Numerical
  Investigation of the Effect of Geometric Design Parameters on Swirl Brake
  Performance,” SciTech 2017, Grapevine, Texas by N. R. Matula and
  P. G. A. Cizmas.
6. ”Effect
  of Gradient Reconstruction Method on Transonic Fan Performance,”
  SciTech 2017, Grapevine, Texas by F. Carpenter and P. G. A. Cizmas.
7. ”Proper Orthogonal Decomposition Applied to a Turbine Stage with
  In-Situ Combustion,” 3rd International Congress on Energy Efficiency and
  Energy Related Materials, Oludeniz, Turkey (2015) by D. Isvoranu,
  S. Danaila, P. Cizmas and C. Leventiu; Springer Proceedings in Energy
  (2017).

2018

1. ”
  Macro-scale fatigue fracture analysis of multiphase bodies, aircraft
  design, and catastrophic failure: Two aircraft accidents,”
  Engineering Fracture Mechanics, 199, 274–279 (2018) by J. C. Slattery and
  P. G. A. Cizmas.
2. ”A
  method for generating reduced-order combustion mechanisms that satisfy the
  differential entropy inequality,” Physics of Fluids, 30, 4,
  043601-1–17 (2018) by A. E. Ream, J. C. Slattery and P. G. A. Cizmas.
3. ”
  A Reduced-Order Methane-Air Combustion Mechanism that Satisfies the
  Differential Entropy Inequality,” Proceedings of the Romanian
  Academy, Series A, 193–198, (2018) by A. E. Ream, J. C. Slattery and
  P. G. A. Cizmas.
4. ”A
  reduced-order model for compressible flows based on an efficient proper
  orthogonal decomposition method,” Proceedings of the 15th
  International Symposium on Unsteady Aerodynamics, Aeroacoustics &
  Aeroelasticity of Turbomachines, University of Oxford, UK, September 24-27
  (2018) by E. H. Krath, J. A. Felderhoff, N. R. Matula, P. G. A. Cizmas and
  D. A. Johnston.
5. ”The
  second law of thermodynamics and the numerical simulation of transport
  phenomena with chemical reactions,” Tenth International Conference on
  Computational Fluid Dynamics (ICCFD10), ICCFD10-2018-0360, Barcelona,
  Spain, July 9–13 (2018) by P. G. A. Cizmas, J. C. Slattery and Allen
  E. Ream.

2019

1. ”A Multi-Fidelity Optimization Study Investigating Distributed
  Adaptivity for Robust Low-Boom Performance,” AIAA Aviation &
  Aeronautics Forum & Exposition, Dallas, Texas, May 17-21 (2019) by
  F. L. Carpenter, P. G. A. Cizmas, C. R. Bolander, T. N. Giblette, and
  D. F. Hunsaker.
2. ”Achieving Quieter Supersonic Flight Through Outer-Mold Line
  Modification: An Optimization Study,” AIAA Aviation & Aeronautics
  Forum & Exposition, Dallas, Texas, May 17-21 (2019) by S. R. Reddy,
  G. S. Dulikravich, F. L. Carpenter, and P. G. A. Cizmas.
3. ”Reduced-Order Model of Unsteady Flows in a Turbomachinery Fan Modeled
  using a Novel Proper Orthogonal Decomposition,” ASME Turbo Expo 2019,
  Phoenix, Arizona, May 17-21 (2019) by E. H. Krath, F. L. Carpenter,
  P. G. A. Cizmas, and D. A. Johnston.
4. ”Controlling
  Sonic Boom Loudness Through Outer Mold Line Modification: A Sensitivity
  Study,” SciTech 2019, San Diego, California by F. L. Carpenter,
  P. G. A. Cizmas, S. R. Reddy and G. S. Dulikravich.

2020

”UNS3D
Simulations for the Third Sonic Boom Prediction Workshop Part I: Biconvex
9×7 Shock-Plume Interaction Model,”AIAA Aviation Forum, Virtual Event,
June 15-19 (2020) by J. Kassing, F. L. Carpenteer and P. G. A. Cizmas.
”UNS3D
Simulations for the Third Sonic Boom Prediction Workshop Part II: C608
Low-Boom Flight Demonstrator,”AIAA Aviation Forum, Virtual Event, June
15-19 (2020) by F. L. Carpenteer and P. G. A. Cizmas.
”Analysis
of Turbine Viscous Flow Using a Novel Proper Orthogonal Decomposition
Method,”AIAA Propulsion and Energy Forum, Virtual Event, August 24-28
(2020) by E. H. Krath, F. L. Carpenteer and P. G. A. Cizmas.