Non-Arrhenius NO Formation Rate in One-Dimensional Nozzle Airflow
Author:
Affiliation:
1. Consiglio Nazionale delle Ricerche, 70126 Bari, Italy
2. ESA, 2200 AG Noordwijk, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.6448
Reference10 articles.
1. 1Park, C., Non-Equilibrium Hypersonic Aerothermodynamics, Wiley, New York, 1990, pp.326, 327.
2. Nonequilibrium vibrational kinetics in the boundary layer of re-entering bodies
3. Electron and vibrational kinetics in the boundary layer of hypersonic flow
4. State-to-State Approach in the Kinetics of Air Components Under Re-Entry Conditions
5. Thermal rate constants of the N2+O→NO+N reaction using ab initio 3A″ and 3A′ potential energy surfaces
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