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ANALYSIS OF DUAL BELL ROCKET NOZZLE USING COMPUTATIONAL FLUID DYNAMICS

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ANALYSIS OF DUAL BELL ROCKET NOZZLE USING COMPUTATIONAL FLUID DYNAMICS

ORDINARY APPLICATION

Published

date

Filed on 12 September 2023

Patent Information

Application ID202341061197
Date of Application12/09/2023

Documents

NameDate
202341061197-COMPLETE SPECIFICATION [12-09-2023(online)].pdf12/09/2023
202341061197-DRAWINGS [12-09-2023(online)].pdf12/09/2023
202341061197-FIGURE OF ABSTRACT [12-09-2023(online)].pdf12/09/2023
202341061197-FORM 1 [12-09-2023(online)].pdf12/09/2023
202341061197-FORM-9 [12-09-2023(online)].pdf12/09/2023
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