The objective of the current work is to develop an non-intrusive technique to experimentally determine the major species and temperature field in the combustion chamber of a uni-element rocket for a GO2/GH2 propellant combination.
Spatially Resolved Species Measurements in a GO2/GH2 Propellant Rocket
1996-03-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Spatially Resolved Species Measurements in a GO~2/GH~2 Propellant Rocket
British Library Conference Proceedings | 1996
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