Static pressure distributions along the launcher wall and pitot pressure measurements from the annular region between the rocket and the launcher were made as an underexpanded supersonic nozzle exhausted into an expansive launch tube. The flow remained supersonic along the entire length of the launcher for all nozzle locations studied.
Flow field for an underexpanded, supersonic nozzle exhausting into an expansive launch tube
1976-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Flow Separation Inside a Supersonic Nozzle Exhausting into a Subsonic Compressible Crossflow
Online Contents | 2003
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