All Stories

  1. Effects of supersonic boundary layer combustion on wall shear stress and heat transfer

    Article • Aerospace Science and Technology, December 2026, Elsevier

    Dr. Yunpeng Wang

  2. Aerodynamic–Control–Trajectory Collaborative Optimization Methods for Hypersonic Reusable Vehicles

    Article • Aerospace Science and Technology, August 2026, Elsevier

    Dr. Yunpeng Wang

  3. Development of pulse-type skin friction balance use in shock tunnel

    Article • Review of Scientific Instruments, April 2025, American Institute of Physics

    Dr. Yunpeng Wang

  4. An oscillation flow mechanism of hypersonic flows over parallel-staged double-wedge configuration

    Article • Physics of Fluids, February 2025, American Institute of Physics

    Dr. Yunpeng Wang

  5. Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration

    Article • Physics of Fluids, January 2024, American Institute of Physics

    Dr. Yunpeng Wang

  6. Force measurement using strain-gauge balance in shock tunnel based on deep learning

    Article • Chinese Journal of Aeronautics, August 2023, Tsinghua University Press

    Dr. Yunpeng Wang

  7. Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle

    Article • Physics of Fluids, May 2023, American Institute of Physics

    Dr. Yunpeng Wang

  8. Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle

    Article • Journal of Spacecraft and Rockets, January 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Yunpeng Wang

  9. Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel

    Article • AIAA Journal, December 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Yunpeng Wang

  10. Theories and methods for designing hypersonic high-enthalpy flow nozzles

    Article • Chinese Journal of Aeronautics, January 2022, Elsevier

    Dr. Yunpeng Wang

  11. Intelligent Force-Measurement System Use in Shock Tunnel

    Article • Sensors, October 2020, MDPI AG

    Dr. Yunpeng Wang

  12. Impulse force-measurement system

    Article • Shock Waves, September 2020, Springer Science + Business Media

    Dr. Yunpeng Wang

  13. Starting Process in a Large-Scale Shock Tunnel

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

    Dr. Yunpeng Wang, Dr. Zongmin HU, Zonglin Jiang, yunfeng liu

  14. Numerical Investigation of the Starting Process in a Long-test-duration Hypervelocity Shock Tunnel

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

    Dr. Yunpeng Wang, Dr. Zongmin HU, Zonglin Jiang, yunfeng liu

  15. Abort Separation of Launch Escape System Using Aerodynamic Interference

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

    Dr. Yunpeng Wang

  16. Numerical Investigation of Supersonic Oscillatory Flow with Strong Interference over a Capsule-shaped Abort System

    Article • TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2012, Japan Society for Aeronautical and Space Sciences

    Dr. Yunpeng Wang

  17. Improvement in Capsule Abort Performance Using Supersonic Aerodynamic Interaction by Fences

    Article • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2012, Japan Society for Aeronautical and Space Sciences

    Dr. Yunpeng Wang

  18. Simulation of Supersonic Stage Separation of Capsule-Shaped Abort System by Aerodynamic Interaction

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

    Dr. Yunpeng Wang

  19. Supersonic Unsteady Flow Around a Capsule-Shaped Abort System with Angle of Attack

    Article • International Journal of Aerospace and Lightweight Structures (IJALS) -, January 2011, Research Publishing Services

    Dr. Yunpeng Wang

  20. Supersonic Unsteady Flow Around a Capsule-Shaped Abort System with Angle of Attack

    Article • International Journal of Aerospace and Lightweight Structures (IJALS) -, January 2011, Research Publishing Services

    Dr. Yunpeng Wang