Combustion Based Fluidic Propulsion System: A Novel Approach to Integrated Wing Propulsion

This paper presents a novel combustion-based fluidic propulsion system designed for integration within an aerodynamic wing structure. [cite: 872, 873, 874] The system utilizes controlled combustion of fuel-air mixtures within the wing to generate thrust, capitalizing on aerodynamic principles and fluidic amplification. [cite: 875, 876, 877] A prototype system is developed, and key performance parameters, including thrust, pressure dynamics, and flame stability, are analyzed. [cite: 924, 925, 926, 927] The results demonstrate the potential of this integrated approach for enhancing propulsion efficiency and reducing drag in low-scale propulsion applications.