Optimization of combustion and performance parameters by intake-charge conditions in a small-scale air-cooled hydrogen fuelled SI engine suitable for use in piston-prop aircraft


GÜRBÜZ H.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2020 (SCI-Expanded) identifier identifier

  • Publication Type: Article / Article
  • Volume:
  • Publication Date: 2020
  • Doi Number: 10.1108/aeat-09-2020-0193
  • Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus, Academic Search Premier, ABI/INFORM, Aerospace Database, Compendex, INSPEC
  • Keywords: Engine performance, Hydrogen SI engine, In-cylinder combustion, Intake-charge conditions, NOx emission, EXHAUST-GAS RECIRCULATION, SPARK-IGNITION ENGINE, NOX EMISSION REDUCTION, COMBINED INJECTION, HYDROGEN/GASOLINE, BACKFIRE, MIXTURE, CYCLE
  • Süleyman Demirel University Affiliated: Yes

Abstract

Purpose