This citation summarizes a one-page announcement of technology available for utilization. A proposal for steading the flow from the rocket nozzle on the Space Shuttle main engine could be applied to other large-area-ration contoured nozzles. Oscillations and pulsations in the boundary-layer flow would be reduced by flaring the nozzle exit. Transient side loads on the nozzle would be suppressed. ...FOR ADDITIONAL INFORMATION: Contact: Director, Technology Transfer Division, P.O. Box 8757, BWI Airport, MD 21240. Refer to MFS-19567/DB.
Nozzle Modification Suppresses Flow Transients: Fluctuations in boundary-layer flow would be reduced by flaring the nozzle exit
1982
1 pages
Report
No indication
English
Nozzle Modification Suppresses Flow Transients
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