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  1. A Machine Learning Approach to Predicting Unsteady Transonic Flow of Pitching Airfoils

    Article • Journal of Fluids Engineering, October 2022, ASME International

    Dr Upender K Kaul

  2. An Active Flow Control Approach for Spatially Growing Mixing Layer

    Article • Journal of Fluids Engineering, March 2022, ASME International

    Dr Upender K Kaul

  3. Resolving Pitching Airfoil Transonic Aerodynamics by Computational Fluid Dynamics Data Modeling1

    Article • Journal of Fluids Engineering, May 2021, ASME International

    Dr Upender K Kaul

  4. Extending A Correction Method for Unsteady Transonic Aerodynamics to Variable Camber Continuous Trailing Edge Flap

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr Upender K Kaul

  5. RANS simulations of a pitching and plunging VCCTEF airfoil toward a transonic flutter model

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul, Dr Nhan Nguyen

  6. Flutter Analysis of the Transonic Truss-Braced Wing Aircraft Using Transonic Correction

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr Upender K Kaul, Jason Fugate

  7. Lift Characterization Study of a Two-Element Three-Segment Variable Camber Airfoil

    Article • June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  8. Drag Characterization Study of Variable Camber Continuous Trailing Edge Flap

    Article • Journal of Fluids Engineering, May 2018, ASME International

    Dr Upender K Kaul

  9. Semisupervised Learning of Lift Optimization of Multi-Element Three-Segment Variable Camber Airfoil

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  10. Lift Optimization Study of a Multi-Element Three-Segment Variable Camber Airfoil

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul, Dr Nhan Nguyen

  11. Development of Variable Camber Continuous Trailing Edge Flap for Performance Adaptive Aeroelastic Wing

    Article • September 2015, SAE International

    Dr Upender K Kaul

  12. A 3-D Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr Upender K Kaul

  13. Mixing Layer: Numerical and Experimental Control Strategies

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  14. Optimization of Perturbation Parameters for Simulated Free Shear Layer Flow

    Article • International Journal of Flow Control, December 2014, Portico

    Dr Upender K Kaul

  15. First Principles Based PID Control of Mixing Layer: Role of Inflow Perturbation Spectrum

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  16. Optimization of Perturbation Parameters for Simulated Free Shear Layer Flow

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  17. Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Nhan Nguyen, Dr Upender K Kaul

  18. An Efficient CFD-based PID Control of Free Shear Layer Flow

    Article • June 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  19. Stability Enhanced High-Order Hyperviscosity-Based Shock Capturing Algorithm

    Article • AIAA Journal, June 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  20. Skin-Friction Predictions on a Hovering Tilt-Rotor Blade

    Article • Journal of Aircraft, November 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  21. Skin Friction Predictions over a Hovering Tilt-Rotor Blade Using OVERFLOW2

    Article • June 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  22. A High-Order Dissipative Scheme for the Hyperviscosity-Based Shock-Capturing Algorithm

    Article • June 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  23. Effect of Inflow Boundary Conditions on the Turbulence Solution in Internal Flows

    Article • AIAA Journal, February 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  24. Three-dimensional elliptic grid generation with fully automatic boundary constraints

    Article • Journal of Computational Physics, August 2010, Elsevier

    Dr Upender K Kaul

  25. Effect of Inflow Boundary Conditions on the Solution of Transport Equations for Internal Flows

    Article • June 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  26. New Dissipative Leapfrog Finite Difference Scheme for Elastodynamic Simulation in Noninertial Frames

    Article • AIAA Journal, August 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  27. Three-Dimensional Elliptic Grid Generation with Fully Automatic Boundary Constraints

    Article • June 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  28. Modeling and Simulation of Normal and Damage Vibration Signatures of Idealized Gears

    Article • Structural Health Monitoring, April 2008, SAGE Publications

    Dr Upender K Kaul

  29. Idealized Modeling and Analysis of the Shuttle Orbiter Wing Leading Edge Impact Data

    Article • September 2007, SAE International

    Dr Upender K Kaul

  30. Machine Learning for Detecting and Locating Damage in a Rotating Gear

    Article • October 2005, SAE International

    Dr Upender K Kaul

  31. New boundary constraints for elliptic systems used in grid generation problems

    Article • Journal of Computational Physics, August 2003, Elsevier

    Dr Upender K Kaul

  32. Detection and diagnosis of changes in the time-scale eigenstructure for vibrating systems

    Article • January 2001, Institute of Electrical & Electronics Engineers (IEEE)

    Dr Upender K Kaul

  33. Full viscous modeling in generalized coordinates of heat conducting flows in rotating systems

    Article • Journal of Thermophysics and Heat Transfer, October 1996, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  34. Full viscous modeling in generalized coordinates of heat conducting flows in rotating systems

    Article • June 1993, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  35. On Some Aspects of Wave Interactions in Plane Mixing Layers

    Article • January 1989, Springer Science + Business Media

    Dr Upender K Kaul

  36. Do large structures control their own growth in a mixing layer? An assessment

    Article • Journal of Fluid Mechanics, May 1988, Cambridge University Press

    Dr Upender K Kaul

  37. On the accuracy of the pseudocompressibility method in solving the incompressible Navier-Stokes equations

    Article • Applied Mathematical Modelling, February 1987, Elsevier

    Dr Upender K Kaul

  38. Computation of internal turbulent flow with a large separated flow region

    Article • International Journal for Numerical Methods in Fluids, December 1986, Wiley

    Dr Upender K Kaul

  39. A relaxation technique for the parabolized Navier-Stokes (PNS) equations

    Article • Communications in Applied Numerical Methods, November 1986, Wiley

    Dr Upender K Kaul

  40. A numerical study of three-dimensional incompressible flow around multiple posts

    Article • January 1986, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  41. A wind tunnel inlet flow simulation

    Article • Journal of Aircraft, October 1985, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  42. On the accuracy of the pseudocompressibility method in solving the incompressible Navier-Stokes equations

    Article • July 1985, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  43. Computations of internal turbulent flow with large separated flow regions

    Article • July 1985, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  44. A computational study of saddle point separation and horseshoe vortex system

    Article • January 1985, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  45. A numerical simulation of the NFAC (National Full-scale AerodynamicsComplex) open-return wind tunnel inlet flow

    Article • January 1985, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  46. A comparative study of the parabolized Navier-Stokes code using various grid-generation techniques

    Article • Computers & Fluids, January 1985, Elsevier

    Dr Upender K Kaul

  47. A comparative study of the parabolized Navier-Stokes code using various grid-generation techniques

    Article • January 1984, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Upender K Kaul

  48. A numerical method to assess the feedback in a free shear layer

    Article • Springer Science + Business Media

    Dr Upender K Kaul

  49. A numerical study of incompressible juncture flows

    Article • Springer Science + Business Media

    Dr Upender K Kaul

  50. Time-scale local approach for vibration monitoring

    Article • Institute of Electrical & Electronics Engineers (IEEE)

    Dr Upender K Kaul