Quantitative estimation of the static and dynamic parameters of jet a-air combustion and detonation from the first principles calculations.
Conference
·
OSTI ID:977016
The Jet A surrogate, consisted from 72.7 wt % decane + 9.1 wt % hexane + 18.2 wt % benzene was selected. Detailed mechanism, consisted of 417 elementary reversible reactions and 71 components, for this Jet A surrogate combustion was elaborated. The capability of the 3-component Jet A surrogate to predict the ignition delay times for the Jet A fuel over wide temperature and pressure ranges and to predict the pressure, temperature, and velocity of detonation was demonstrated.
- Research Organization:
- Argonne National Lab. (ANL), Argonne, IL (United States)
- Sponsoring Organization:
- USDOE National Nuclear Security Administration (NNSA)
- DOE Contract Number:
- DE-AC02-06CH11357
- OSTI ID:
- 977016
- Report Number(s):
- ANL/NE/CP-58581; TRN: US201009%%24
- Resource Relation:
- Conference: 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibition; Jul. 8, 2007 - Jul. 11, 2007; Cincinnati, OH
- Country of Publication:
- United States
- Language:
- ENGLISH
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