Conference proceeding
Shock Tube Measurements of Jet and Rocket Fuels
American Institute of Aeronautics and Astronautics. AIAA Meeting Papers
AIAA Aerospace Sciences Meeting, 54 (San Diego, California, 01/04/2016–01/08/2016)
01/01/2016
Handle:
https://hdl.handle.net/2376/121252
Appears in Aviation Sustainability Center (ASCENT)
Abstract
A database of ignition delay times and pyrolysis product species time-histories was acquired for a variety of jet fuels and rocket propellants. These ignition delay times and laser absorption data are characterized by very accurate and uniform test conditions, fuel loading and species concentrations. Ignition delay times were measured over temperatures from 700 to 1700 K. Species concentrations during pyrolysis were measured over temperatures from 1100 to 1600 K. These species time-history data and ignition delay times provide kinetic targets for jet and rocket fuel models and can be used to constrain reduced pyrolysis sub-mechanisms found in hybrid models.
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Details
- Title
- Shock Tube Measurements of Jet and Rocket Fuels
- Creators
- David F. Davidson - Stanford UniversityYangye Zhu - Stanford UniversityShengkai Wang - Stanford UniversityThomas Parise - Stanford UniversityRito Sur - Stanford UniversityRonald K. Hanson - Stanford University
- Publication Details
- American Institute of Aeronautics and Astronautics. AIAA Meeting Papers
- Conference
- AIAA Aerospace Sciences Meeting, 54 (San Diego, California, 01/04/2016–01/08/2016)
- Academic Unit
- Aviation Sustainability Center (ASCENT); Alternative Jet Fuel
- Publisher
- American Institute of Aeronautics and Astronautics
- Identifiers
- 99900621899801842
- Language
- English
- Resource Type
- Conference proceeding