Problems facing the National Aerospace Plane (NASP) nozzle at transonic and low supersonic conditions are discussed. An overview of NASP nozzle research at Lewis Research Center is given. Experimental facilities and computational techniques currently in use are reviewed. External burning as a means to reduce transonic drag and initial results of external burning experiments are discussed.
Overview of NASP Nozzle Research
1991
16 pages
Report
No indication
English
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