Shock Tube Study of Methylcyclohexane Ignition over a Wide Range of Pressure and Temperature

Author:

Vasu Subith S.1,Davidson David F.1,Hong Zekai1,Hanson Ronald K.1

Affiliation:

1. Mechanical Engineering Department, Stanford University, Stanford, California 94305

Publisher

American Chemical Society (ACS)

Subject

Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering

Reference76 articles.

1. Jet fuel ignition delay times: Shock tube experiments over wide conditions and surrogate model predictions

2. Colket, M.; Edwards, T.; Williams, S.; Cernansky, N. P.; Miller, D. L.; Egolfopoulos, F.; Lindstedt, P.; Seshadri, K.; Dryer, F. L.; Law, C. K.; Friend, D.; Lenhert, D. B.; Pitsch, H.; Sarofim, A.; Smooke, M.; Tsang, W.In 45th American Institute of Aeronautics and Astronautics (AIAA) Aerospace Sciences Meeting, Reno, NV,2007; paper AIAA 2007-0770.

3. Surrogate Mixtures to Represent Complex Aviation and Rocket Fuels

4. Edwards, T.In 38th American Institute of Aeronautics and Astronautics (AIAA)/American Society of Mechanical Engineers (ASME)/Society of Automotive Engineers (SAE)/American Society for Engineering Education (ASEE) Joint Propulsion Conference, Indianapolis, IN,2002; paper AIAA-2002-3874.

5. Liquid Fuels and Propellants for Aerospace Propulsion: 1903-2003

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