Thermomechanical Characterization of Hot Surface Ignition Device Using Phenomenological Heat Flux Model
Author:
Funder
Army Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38662
Reference33 articles.
1. Diesel, Spark-Ignition, and Turboprop Engines for Long-Duration Unmanned Air Flights
2. Knock criteria for aviation diesel engines
3. RyuJ. I.MotilyA. H.LeeT.ScarcelliR.SomS.KimK. S.KweonC.B. M. “Ignition Enhancement of F-24 Jet Fuel by a Hot Surface for Aircraft Propulsion Systems,” AIAA Paper 2020-2142, Jan. 2020. 10.2514/6.2020-2142
4. MotilyA. H.RyuJ. I.KimY.KimK. S.LeeT.KweonC.B. M. “Effects of Cetane Number on High-Pressure Fuel Spray Characteristics with a Hot Surface Ignition Source,” AIAA Paper 2020-2280, Jan. 2020. 10.2514/6.2020-2280
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