Beijing, China

Jian Pang


Average Co-Inventor Count = 12.0

ph-index = 1


Company Filing History:


Years Active: 2025

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1 patent (USPTO):

Title: Innovations of Jian Pang in High-Enthalpy Shock Tunnel Diagnostics

Introduction

Jian Pang is a notable inventor based in Beijing, China. He has made significant contributions to the field of aerospace aerodynamics, particularly in diagnosing high-enthalpy shock tunnel parameters. His innovative approach combines advanced measurement technologies to enhance the understanding of flow field dynamics.

Latest Patents

Jian Pang holds a patent for a "Method and system for diagnosing high-enthalpy shock tunnel parameters." This invention provides a comprehensive method for diagnosing the flow field parameters of high-enthalpy shock tunnels. The method utilizes both contact measurement technology and non-contact spectrum measurement technology to accurately assess various parameters, including flow field temperature, pressure, and component concentrations. Additionally, it captures non-equilibrium state information and effective wind tunnel working time, which are crucial for aerospace research and development.

Career Highlights

Jian Pang is affiliated with the China Academy of Aerospace Aerodynamics, where he applies his expertise in aerodynamics and flow diagnostics. His work has been instrumental in advancing the understanding of high-enthalpy flow fields, which are critical for various aerospace applications. His innovative methods have the potential to improve the efficiency and accuracy of aerodynamic testing.

Collaborations

Jian Pang has collaborated with esteemed colleagues such as Junmou Shen and Meixiao Hu. These collaborations have fostered a productive research environment, leading to advancements in the field of aerospace aerodynamics.

Conclusion

Jian Pang's contributions to the field of high-enthalpy shock tunnel diagnostics exemplify the importance of innovation in aerospace research. His patented methods and collaborative efforts continue to push the boundaries of what is possible in aerodynamics.

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