All Stories

  1. Three-Dimensional Pitching Panel Wake: Lagrangian Analysis and Momentum Distribution from Experiments

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

    Dr Rajeev Kumar

  2. Experimental study on the effects of trailing edge geometry on the wake structure of a trapezoidal pitching panel

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Rajeev Kumar

  3. Three-Dimensional Finite-Time Lyapunov Exponent Field in the Wake of an Oscillating Trapezoidal Pitching Panel

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Rajeev Kumar

  4. The momentum field created by a bio-inspired pitching panel.

    Article • Marine Technology Society Journal, September 2016, Marine Technology Society

    Dr Rajeev Kumar

  5. PIV measurements behind a bio-inspired pitching panel modeling fish fin.

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

    Dr Rajeev Kumar

  6. Numerical Analysis of Transient Temperature Distribution in a Partially Cooled Nuclear Fuel Rod

    Article • November 2015, ASME International

    Dr Rajeev Kumar

  7. Simultaneous measurement of aerodynamic forces and kinematics in flapping wings of tethered locust

    Article • Bioinspiration & Biomimetics, October 2015, Institute of Physics Publishing

    Dr Rajeev Kumar

  8. Kinematics and Inertial Effects in Locust Flapping Wings

    Article • Experimental Mechanics, September 2015, Springer Science + Business Media

    Dr Rajeev Kumar

  9. Kinematic and Aerodynamic Response of Locusts in Sideslip

    Article • International Journal of Micro Air Vehicles, June 2015, SAGE Publications

    Dr Rajeev Kumar

  10. Kinematics and Inertial Effects in Locust Flapping Wings

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

    Dr Rajeev Kumar

  11. Instantaneous Forces in Locust Flapping Wings

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

    Dr Rajeev Kumar

  12. INSECT-INSPIRED MICRO AIR VEHICLES

    Article • April 2014, World Scientific Pub Co Pte Lt

    Dr Rajeev Kumar

  13. Kinematics and Aerodynamic Response of Locusts in Sideslip

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

    Dr Rajeev Kumar

  14. Force Measurements on Locusts during Visually-Evoked Collision Avoidance Maneuvers

    Article • International Journal of Micro Air Vehicles, September 2012, SAGE Publications

    Dr Rajeev Kumar

  15. Effects of Yaw Angle on Aerodynamic Response in Locusts

    Article • January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Rajeev Kumar

  16. Experimental Study of Aerodynamic Performance of Locust and Model Wings

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

    Dr Rajeev Kumar

  17. The Least-Squares Galerkin Split Finite Element Method for Buoyancy-Driven Flow

    Article • January 2010, ASME International

    Dr Rajeev Kumar

  18. A Least-Squares Galerkin Split Finite Element Method for Compressible Navier-Stokes Equations

    Article • January 2009, ASME International

    Dr Rajeev Kumar

  19. Marriage of least-squares and Galerkin FEM to solve Inompressible flows.

    Article • January 2008, ASME International

    Dr Rajeev Kumar

  20. Bubble-Enriched Least-Squares Finite Element Method for Transient Advective Transport

    Article • Differential Equations and Nonlinear Mechanics, January 2008, Hindawi Publishing Corporation

    Dr Rajeev Kumar

  21. Drag Reduction Due to Riblets on a GAW(2) Airfoil

    Article • Journal of Aircraft, September 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Rajeev Kumar