Dr. Nematollah Fouladi is an accomplished aerospace engineer and an innovative researcher whose scientific vision and technical mastery have significantly contributed to advancements in the field of aerospace propulsion and fluid dynamics. He currently serves as a Researcher at the Iranian Space Research Center, Tehran, where he leads and collaborates on cutting-edge projects focusing on high-altitude testing facilities, supersonic exhaust diffusers, and aerodynamic system optimization. Dr. Fouladi obtained his Ph.D. in Aerospace Engineering from Sharif University of Technology, Tehran, one of the most prestigious engineering universities recognized for its excellence in research and education. His academic journey has been distinguished by a strong focus on computational and experimental fluid mechanics, turbulence modeling, and supersonic flow control, all of which reflect his unwavering dedication to precision and scientific advancement. Throughout his career, Dr. Fouladi has demonstrated outstanding analytical and research capabilities, successfully integrating advanced simulation techniques with practical experimentation to develop efficient and reliable aerospace propulsion systems. His research interests lie primarily in the areas of aerothermodynamics, gas dynamics, high-altitude testing methodologies, and aerospace cooling system design, which play a critical role in improving the performance, safety, and sustainability of aerospace technologies. In addition to his technical expertise, Dr. Fouladi exhibits a strong command of numerical modeling, data interpretation, computational fluid dynamics (CFD), heat transfer analysis, and system integration, enabling him to contribute to interdisciplinary collaborations within international research networks. As an active contributor to scholarly communication, Dr. Nematollah Fouladi has authored 18 documents, garnered 109 citations, and achieved an h-index of 6, demonstrating his growing influence and recognition in the global aerospace research community. His works are published in leading peer-reviewed journals such as Physics of Fluids, Acta Astronautica, Aerospace Science and Technology, and Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. These publications have provided valuable insights into high-speed flow behavior, diffuser performance, and nozzle optimization—offering practical solutions to aerospace challenges faced by industry and research institutions alike. Dr. Fouladi’s commitment extends beyond research as he actively participates in collaborative engineering projects, contributing to advancements in Iran’s aerospace infrastructure and capacity-building initiatives. His professional experience also includes involvement in experimental investigations that support national and international aerospace objectives, reinforcing his reputation as a reliable and forward-thinking engineer. He has demonstrated leadership qualities through mentoring emerging researchers, fostering innovation-driven research environments, and promoting scientific excellence across disciplines. Dr. Fouladi’s research skills encompass a comprehensive blend of theoretical analysis, computational proficiency, and experimental design—qualities that make his work both academically robust and practically relevant. His contributions have been recognized by academic and research communities, earning him honors and respect as a key figure in aerospace technology development.

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Featured Publications

1. Fouladi, N. (2025). Cooling system design and analysis for high heat flux large dimension diffuser of a high-altitude test facility. International Journal of Thermofluids. (Cited by 5)

2. Fouladi, N. (2024). Experimental evaluation of the influence of the diffuser inlet to nozzle exit cross sectional area ratio on pressure oscillation in a high-altitude test facility. Physics of Fluids. (Cited by 7)

3. Fouladi, N. (2024). Gas dynamics at starting and terminating phase of a supersonic exhaust diffuser with a conical nozzle. Physics of Fluids. (Cited by 9)

4. Fouladi, N. (2023). Experimental and comprehensive investigation of second throat diffuser area effect on ground test of a thrust optimized parabolic nozzle with different expansion ratios. Acta Astronautica. (Cited by 10)

5. Fouladi, N. (2023). Starting transient analysis of second throat exhaust diffuser in high-altitude test of a thrust optimized parabolic nozzle. Physics of Fluids. (Cited by 6)