Measurement and analysis of transient hydrogen injection rates from pintle-type injector in choked flow conditions
The transient variation of fuel injection rate is a critical factor affecting mixture formation and combustion phase as well as the energy supply rate in direct-injection engines. Despite its great importance, transient injection rates of hydrogen direct-injection injectors have rarely been characterized previously under various injector operating conditions considering injector dynamics. The current study measures and analyzes the transient injection rates of a pintle-type hydrogen injector under various injection and ambient pressures in choked flow conditions and examines the predictability of transient injection rates based on the compressible flow theory of converging-diverging nozzles and pintle dynamics. The transient injection rate profile is obtained by measuring the jet force at the nozzle exit and calibrating it to the time-averaged mass flow rate data. An increase in injection pressure caused a steeper rising slope of injection rate and a longer total injection duration with a linear increase in quasi-steady injection rate. As the ambient pressure increased, the rising slope of the injection rate and the total injection duration decreased, while the quasi-steady injection rate remained nearly the same. These transient and quasi-steady injection rate characteristics were able to be predicted based on the mass flow rate equation of converging-diverging nozzles in choked flow conditions and the transient pintle stroke as the input parameter.
Authors
- Gyuhan Bae (ORCID: https://orcid.org/0000-0001-7276-9896)
- Seoksu Moon (ORCID: https://orcid.org/0000-0003-0316-5292)
- Jaehyun Lee (ORCID: https://orcid.org/0009-0008-1003-5465)
Institutions
- Inha University (KR)
Publication Details
- Journal
- Case Studies in Thermal Engineering
- Published
- 2026-08-31
- DOI
- https://doi.org/10.1016/j.csite.2026.108471
- Primary Topic
- Advanced Combustion Engine Technologies
- Type
- article
- Field-Weighted Citation Impact
- 0.00