The results of first year's efforts on a experimental base flow program are reported. The design and checkout for a Mach 3.0 axisymmetric wind tunnel with a model base diameter of 2.25 inches is described, as well as the automated data acquisition system. Experiments are reported on detailed static pressures for the diffuser wall, model wall and bases and near wake. Temperature measurements are presented to establish a near adiabatic wall condition. The relationship between the experimental program and propulsive external burning is discussed.
Experiments and analysis related to external burning for propulsion
Experimente und Analysen mit und von aeusserer Verbrennung als Antriebsmittel
US Government Reports ; 1-63
1976
63 Seiten
Report
English
Experiments related external burning for propulsion
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|