What is it about?
A computational model is developed to analyse the flow characteristics of linear plug nozzle and a truncated plug with 40% plug-length, with base bleeds. The performance is seen to improve with the introduction of base bleed. The model will help in identifying and designing altitude adaptive nozzle configuration for launch vehicles.
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This page is a summary of: Numerical Analysis of Flowfield in Linear Plug Nozzle with Base Bleed, Journal of Spacecraft and Rockets, August 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34992.
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