Dr. Feng Guo is a leading researcher in the field of aerospace propulsion and hybrid energy systems, with extensive experience in turbine engines, advanced flight propulsion control, and multi-fuel energy technologies. With a background in integrated aircraft and propulsion system analysis, Dr. Guo has established a strong reputation for bridging theoretical innovation with practical aerospace engineering solutions. His multidisciplinary approach combines aerodynamics, energy conversion, and propulsion system design to address current and future challenges in aviation and sustainable energy systems. A prolific academic with an active presence in international research forums, Dr. Guo’s contributions are well recognized for their depth, relevance, and potential global impact.

Academic Profile:

ORCID

Education:

Dr. Guo earned his doctoral degree in Aerospace Propulsion from a distinguished academic institution known for its excellence in engineering and scientific research. His academic journey was driven by a deep interest in propulsion integration, leading to his specialization in turbine-based combined cycle systems and their performance under real-world operational conditions. During his graduate and postgraduate studies, Dr. Guo developed expertise in propulsion control, hybrid engine systems, and dynamic inlet/engine coupling. His doctoral research laid the foundation for his future work in advanced propulsion optimization and sustainable fuel integration.

Experience:

Dr. Guo has held key research and academic positions at renowned aerospace and engineering organizations, where he has led and participated in numerous high-impact research initiatives. His work focuses on propulsion system optimization, energy-efficient turbine technologies, and hybrid electric engine configurations. He has collaborated on international projects involving hydrogen and ammonia fuel systems, and contributed to experimental and simulation-based studies on turbine film cooling and ramjet performance. In addition to his research, Dr. Guo has actively reviewed publications for top-tier journals and contributed to academic conferences, sharing his insights on innovative propulsion solutions and flight control mechanisms. His experience also includes mentoring students and coordinating interdisciplinary research teams in propulsion and aerodynamics.

Research Interest:

Dr. Guo’s research interests lie in the development and optimization of advanced propulsion systems, including turbine-based combined cycle (TBCC) engines, hybrid electric propulsion, and sustainable fuel technologies such as hydrogen and ammonia. He is particularly focused on the aerodynamic-propulsion integration of aircraft, thrust-matching techniques, and control law design for variable-geometry engines. Another core area of his research involves performance evaluation through simulation and experimental methods, targeting both atmospheric and near-space flight vehicles. Dr. Guo continues to explore solutions that reduce environmental impact while enhancing propulsion efficiency and operational flexibility, positioning his work at the intersection of aerospace innovation and sustainable engineering.

Award:

Dr. Guo has been recognized for his contributions to the aerospace and energy engineering sectors through nominations and acknowledgments in academic and professional circles. His research excellence, collaborative approach, and commitment to addressing complex engineering problems have earned him distinction among peers. He has been an invited reviewer for international scientific journals and is actively involved in engineering societies that promote advanced propulsion technologies and sustainable energy research. Dr. Guo’s achievements reflect not only technical skill but also leadership in driving interdisciplinary research and mentoring future engineers.

Selected Publications:

• Optimization Methodology of Wide-Speed Scramjet Engine Based on Aerodynamic/Control Coupling, Applied Thermal Engineering, published 2025, 23 citations

• Thrust-Matching and Optimization Design of Turbine-Based Combined Cycle Engine with Trajectory Optimization, International Journal of Turbo and Jet Engines, published 2024, 18 citations

• Flight Analysis and Optimization Design of Vectored Thrust eVTOL Based on Cooperative Flight/Propulsion Control, Aerospace Science and Technology, published 2024, 31 citations

• Analysis and Suppression of Thrust Trap for Turbo-Ramjet Mode Transition with the Integrated Optimal Control Method, Aerospace, published 2023, 27 citations

Conclusion:

Dr. Feng Guo has made substantial contributions to the advancement of propulsion and hybrid aerospace systems through a combination of rigorous research, innovative thinking, and collaborative efforts. His work addresses critical challenges in modern aviation, including fuel efficiency, system integration, and the development of environmentally responsible propulsion technologies. With a strong record of high-impact publications, international collaborations, and academic leadership, Dr. Guo continues to influence the direction of aerospace engineering and energy systems research. He remains committed to pursuing transformative solutions that align with the future of sustainable and high-performance aerospace applications.