Evaluating and Benchmarking the Performance of Dual Bell, Plug, and Conical Nozzles for Enhanced Thrust Efficiency in Aerospace Propulsion
Dhiraj Kumar Mandumula
, Sai Nithin Enjamuri
De Laval Nozzle, Rocket Nozzle Design, Bell Nozzle, Plug Nozzle, Conical Nozzle, Thrust Efficiency, Specific Impulse, Pressure Energy, Nozzle Efficiency.
This paper presents a comparative analysis of dual-bell, plug and conical nozzles taking into consideration various factors such as fuel efficiency, specific impulse, exhaust flow pattern, thermal stresses, acoustic impact, complexity of design and manufacturing under different operating conditions by study and review of multiple papers. The aim of this study is to summarize the various configurations of nozzles and contribute to future research by identifying potential design optimizations for specific mission profiles by combining the best features of each nozzle type.
"Evaluating and Benchmarking the Performance of Dual Bell, Plug, and Conical Nozzles for Enhanced Thrust Efficiency in Aerospace Propulsion ", IJSDR - International Journal of Scientific Development and Research (www.IJSDR.org), ISSN:2455-2631, Vol.9, Issue 10, page no.397 - 409, October-2024, Available :https://ijsdr.org/papers/IJSDR2410048.pdf
Volume 9
Issue 10,
October-2024
Pages : 397 - 409
Paper Reg. ID: IJSDR_212617
Published Paper Id: IJSDR2410048
Downloads: 000347094
Research Area: Engineering
Country: Hyderabad, Telangana, India
ISSN: 2455-2631 | IMPACT FACTOR: 9.15 Calculated By Google Scholar | ESTD YEAR: 2016
An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 9.15 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator
Publisher: IJSDR(IJ Publication) Janvi Wave
