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All Outputs (4)

Non-reacting Numerical Simulation of Axisymmetric Trapped Vortex Combustor (2023)
Conference Proceeding
DAKKA, S., Singh, K., Jefferson-Loveday, R., & Serhat, H. (2023). Non-reacting Numerical Simulation of Axisymmetric Trapped Vortex Combustor.

This paper will focus on suitability of trapped vortex combustor as a candidate for gas turbine combustor objective to minimize pressure drop across combustor and investigating aerodynamic performance. Non-reacting simulation of axisymmetric cavity t... Read More about Non-reacting Numerical Simulation of Axisymmetric Trapped Vortex Combustor.

Aerodynamic Design and Exploration of a Blended Wing Body Aircraft at Subsonic Speed (2019)
Journal Article
Dakka, S., & Johnson, O. (2019). Aerodynamic Design and Exploration of a Blended Wing Body Aircraft at Subsonic Speed. International Journal of Aviation, Aeronautics, and Aerospace, 6(5),

Blended Wing Body (BWB) is a novel aircraft concept which provides many different aerodynamic benefits over conventional aircrafts design. This research investigated the BWB design, L/D characteristics, surface pressure distribution and span-wise lif... Read More about Aerodynamic Design and Exploration of a Blended Wing Body Aircraft at Subsonic Speed.

Aerospace Sealing Technology for Maintenance, Repair and Overhaul of Engines: a Review (2019)
Conference Proceeding
Shabbir, S., Garvey, S., & Dakka, S. M. (2019). Aerospace Sealing Technology for Maintenance, Repair and Overhaul of Engines: a Review.

Given the current rate of growth of gas turbine engines in the aerospace industry, the development of efficient and advanced sealing technology to cater to the harsh operating conditions of the aero-engines is crucial. In addition to developing low-l... Read More about Aerospace Sealing Technology for Maintenance, Repair and Overhaul of Engines: a Review.

Design of power, propulsion, and thermal sub-systems for a 3U CubeSat measuring Earth’s radiation imbalance (2018)
Journal Article
Claricoats, J., & Dakka, S. M. (2018). Design of power, propulsion, and thermal sub-systems for a 3U CubeSat measuring Earth’s radiation imbalance. Aerospace, 5(2), Article 63. https://doi.org/10.3390/aerospace5020063

The paper presents the development of the power, propulsion, and thermal systems for a 3U CubeSat orbiting Earth at a radius of 600 km measuring the radiation imbalance using the RAVAN (Radiometer Assessment using Vertically Aligned NanoTubes) payloa... Read More about Design of power, propulsion, and thermal sub-systems for a 3U CubeSat measuring Earth’s radiation imbalance.