NASA Technical Reports Server (NTRS) 19820010442: Improvement of Rocket Engine Plume Analysis TechniquesReport as inadecuate



 NASA Technical Reports Server (NTRS) 19820010442: Improvement of Rocket Engine Plume Analysis Techniques


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A nozzle plume flow field code was developed. The RAMP code which was chosen as the basic code is of modular construction and has the following capabilities: two phase with two phase transonic solution; a two phase, reacting gas (chemical equilibrium reaction kinetics), supersonic inviscid nozzle-plume solution; and is operational for inviscid solu

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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