Wind-tunnel measurements of ignition delay using shock-induced combustion.
- 1 October 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (10) , 1777-1784
- https://doi.org/10.2514/3.4304
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Atom—Molecule Kinetics at High Temperature Using ESR Detection. Technique and Results for O +H2, O +CH4, and O +C2H6The Journal of Chemical Physics, 1967
- Shock-Tube Study of the Hydrogen—Oxygen Reaction. II. Role of Exchange InitiationThe Journal of Chemical Physics, 1966
- Effects of concentration and of vibrational relaxation on the induction period of the H2−O2 reactionSymposium (International) on Combustion, 1965
- Analytic solutions to the ignition kinetics of the hydrogen-oxygen reactionSymposium (International) on Combustion, 1965
- Determination of induction times in one- dimensional detonations h sub 2, c sub 2 h sub 2, and c sub 2 h sub 4AIAA Journal, 1965
- Structure of gaseous detonation. IV. Induction zone studies in H2-O2 and CO-O2 mixturesSymposium (International) on Combustion, 1965
- Shock-tube study of the hydrogen-oxygen reactionSymposium (International) on Combustion, 1965
- FAST REACTIONS OF OH RADICALSPublished by Elsevier ,1963
- STANDING DETONATION WAVESPublished by Elsevier ,1963
- Kinetic Studies of Hydroxyl Radicals in Shock Waves. III. The OH Concentration Maximum in the Hydrogen-Oxygen ReactionThe Journal of Chemical Physics, 1960