Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts
Abstract
This study examines the combustion and emission behavior of a four-stroke Wankel rotary engine operated in Homogeneous Charge Compression Ignition (HCCI) mode using n-heptane fuel over excess-air ratios of λ = 2.2–2.8. A validated three-dimensional CONVERGE CFD model of the Mazda Renesis RX-8 13B MSP engine—verified against experimental spark-ignition pressure data—was used to assess HCCI performance. The simulations employed semi detailed chemistry (SAGE), Renormalization Group (RNG) k–ε turbulence modelling, and adaptive mesh refinement to capture the multi-stage auto-ignition process. The analysis encompassed key combustion and emission indicators, including in-cylinder and peak pressure, heat-release rate, cumulative heat-release behavior, maximum pressure-rise rate, combustion-phasing metrics crank angle at 10% of total heat released (CA10), crank angle at 50% of total heat released (CA50), crank angle at 90% of total heat released (CA90), combustion duration, and major exhaust species carbon monoxide (CO), carbon dioxide (CO2), hydrocarbons (HC) and nitrogen oxides (NOₓ). Stable HCCI operation was achieved only within a narrow range: λ = 2.2–2.8. Richer mixtures exceeded the 10 bar/°CA knock-related pressure-rise-rate limit, while leaner mixtures resulted in misfire. Increasing λ delayed auto-ignition, weakened high-temperature oxidation, and extended combustion duration. CO and HC emissions rose with λ due to reduced combustion temperature and strong near-wall quenching driven by the Wankel chamber’s high surface-to-volume ratio, whereas NOx remained extremely low and nearly eliminated for λ ≥ 2.4. Overall, the findings confirm that HCCI can be successfully realized in a Wankel rotary engine with ultra-low NOx emissions, provided operation remains within its narrow λ window. These results underscore the potential of Wankel HCCI concepts for lightweight aviation and unmanned aerial vehicle (UAV) propulsion, while highlighting the need for improved mixture preparation and combustion-phasing control for practical implementation.
Keywords
Thanks
The authors thank to Convergent Science for providing CONVERGE Academic licenses and technical support for this work.
References
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Details
Primary Language
English
Subjects
Automotive Combustion and Fuel Engineering
Journal Section
Research Article
Publication Date
December 31, 2025
Submission Date
November 11, 2025
Acceptance Date
December 24, 2025
Published in Issue
Year 2025 Volume: 9 Number: 4
APA
Türkcan, Ö., & Polat, S. (2025). Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts. International Journal of Automotive Science And Technology, 9(4), 626-636. https://doi.org/10.30939/ijastech..1821778
AMA
1.Türkcan Ö, Polat S. Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts. IJASTECH. 2025;9(4):626-636. doi:10.30939/ijastech.1821778
Chicago
Türkcan, Ömer, and Seyfi Polat. 2025. “Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts”. International Journal of Automotive Science And Technology 9 (4): 626-36. https://doi.org/10.30939/ijastech. 1821778.
EndNote
Türkcan Ö, Polat S (December 1, 2025) Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts. International Journal of Automotive Science And Technology 9 4 626–636.
IEEE
[1]Ö. Türkcan and S. Polat, “Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts”, IJASTECH, vol. 9, no. 4, pp. 626–636, Dec. 2025, doi: 10.30939/ijastech..1821778.
ISNAD
Türkcan, Ömer - Polat, Seyfi. “Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts”. International Journal of Automotive Science And Technology 9/4 (December 1, 2025): 626-636. https://doi.org/10.30939/ijastech. 1821778.
JAMA
1.Türkcan Ö, Polat S. Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts. IJASTECH. 2025;9:626–636.
MLA
Türkcan, Ömer, and Seyfi Polat. “Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts”. International Journal of Automotive Science And Technology, vol. 9, no. 4, Dec. 2025, pp. 626-3, doi:10.30939/ijastech. 1821778.
Vancouver
1.Ömer Türkcan, Seyfi Polat. Combustion and Emission Behaviour of a HCCI Wankel Engine Across Lambda Variations: Insights for Future Aviation-Oriented Rotary Engine Concepts. IJASTECH. 2025 Dec. 1;9(4):626-3. doi:10.30939/ijastech. 1821778
