1. 1985

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

  1. 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.
  2. 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.
  3. 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.