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

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.93, sa.3, ss.448-456, 2020 (SCI-Expanded, Scopus)

Yayın Türü: Makale / Tam Makale
Cilt numarası: 93 Sayı: 3
Basım Tarihi: 2020
Doi Numarası: 10.1108/aeat-09-2020-0193
Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus, Academic Search Premier, ABI/INFORM, Aerospace Database, Compendex, INSPEC
Sayfa Sayıları: ss.448-456
Anahtar Kelimeler: 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 Üniversitesi Adresli: Evet

Purpose