The fuel mixing mechanism is a critical aspect of the propulsion system of hypersonic
vehicles. This study aimed to comprehensively investigate a novel jet configuration that …

The efficient injection system has a great role on the overall enactment of air breathing
propulsion systems at supersonic flow. In this work, the usage of extruded multi-injectors in …

This study investigates the influence of a wedge shock generator on hydrogen mixing in an
annular single lobe transverse nozzle at the supersonic combustion chamber of a scramjet …

The main attention of this work is to investigate the usage of diamond multi extruded
injectors on the fuel distribution in combustor of scramjet. This study applied the …

The effect of liquid droplets generated from air-assisted atomization on gas flow
characteristics was studied experimentally. A phase/Doppler particle analyzer was used to …

In present paper, computational fluid dynamic is applied to evaluate hydrogen mixing
impacts of the single extruded lobe injector at supersonic cross flow. The aim of this …

Although fuel spray parameters, such as spray cone angle and penetration length, are
crucial for developing high-efficiency and highperformance combustion engines, general …

The heat transfer phenomenon in the flow of non-Newtonian fluids is important in the
manufacturing processes of plastic products, cooling systems polymer solutions and …

The present paper experimentally verified and computationally explained an improved
design concept of the spray combustion of a gasliquid pintle injector with variable swirl …

Due to the use of Perovskite solar cells (PSC) in aerospace applications, so, in this work for
the first time, aerodynamic flutter and vibrational analysis of PSC are presented. For …