Past Work Expereince

ENGINE COMBUSTION

The methodologies for reducing NOx formation during Hydrogen-Air Combustion

The NOx formation in hydrogen-air combustion in a pulse detonation engines (PDEs) is investigated numerically and validated with experimental data. The calculations are based on axisymmetric Euler equations and a detailed combustion model consisting of 12 species and 27 reactions. A multi-level, dynamically adaptive grid is used to resolve the structure of the detonation front. The calculated NO concentrations were in good agreement with experimental measurements obtained at two operating frequencies and two equivalence ratios. Further calculations studied in detail the effects of equivalence ratio and residence time on NOx formation under ambient conditions. The results show that NOx formation in the PDE is minimized by running lean or rich mixtures and using the shortest possible detonation tubes. NOx emissions for very lean or very rich mixtures are relatively insensitive to residence time. PDE operation at near-stoichiometric equivalence ratios results in very high NOx levels. However, the NOx emission parameter drops significantly for lean or rich mixtures, reaching values comparable to those obtained with current gas turbine engines.

The client needed assistance with the development of five different agricultural aircrafts with diverse configurations such as dual cockpit single control and dual cockpit dual control. Each part, sub-assembly and assemblies, required a certain number of ECNs, which needed to be reflected as individual configuration changes in the model history. Lastly, the client requested the illustrated parts catalog (IPC) connected to their EPDM and linked to its website.

  • Our nine member RGBSI engineering team developed the part models with assemblies comprising different configurations to reflect each ECN change in the individual agricultural aircrafts. Dependent on the configuration of each agricultural aircraft, the part models were installed into different aircraft assemblies, and we checked these assemblies into the IPC and EPDM. Now, when changes are made to the client’s parts or assemblies, they are automatically updated and reflected in the IPC. In addition, the agricultural aircrafts’ IPC pages are convertible to PDF format and linked to a website.
AVATAR
Ariana Grande

Quod autem in homine praestantissimum atque optimum est, id deseruit. Apud ceteros autem philosophos

AEROSPACE & DEFENSE PROJECTS OUR PAST PROJECTS

Related Projects

Engine Combustion We have great problem solving capacity in air and non-air beathing engines combustion with appropreate chemical reactions
Aero & Vibro Acoustics Our main objective was to design a wing which generating low sound pressure level and validate with test data
Store-Separation Having a classical problem solving capacity for 6DOF motion and dynamic motion with grid adaptation techniques.
UAV's Design and developed Drones body with light weight and high strength. and also have done CFD analysis for UAV's, MUAV's, RUAV's.
Hypersonic Intakes CFD analysis of ScramJet engine with design optimization for stoichiometric air-fuel ratio.
Wind Turbine Design and developed most efficient Wind Turbine blade which is more than 5% efficient than existing wing.
Missile Fin Done CFD analysis for load distribution over missile fin and c.g. imbalance.
Missile Nose cone Design and analysis of missile nose cone for lowest possible drag reduction.