All Outputs (12)

A review of novel turbocharger concepts for enhancements in energy efficiency (2010)
Presentation / Conference
Kusztelan, A., Yao, Y., Marchant, D., & Wang, Y. (2010, December). A review of novel turbocharger concepts for enhancements in energy efficiency. Paper presented at International Conference on Energy, Water, and Environment, Amman, Jordan

Development of a multi-block high-order DNS code for turbulent flow simulations (2010)
Presentation / Conference
Castagna, J., & Yao, Y. (2010, July). Development of a multi-block high-order DNS code for turbulent flow simulations. Paper presented at 9th World Congress on Computational Mechanics and 4th Asian Pacific Congress on Computational Mechanics, Sydney, Australia

Measurement and prediction of water coverage of blade ring in a turbocharger (2010)
Conference Proceeding
Yao, J., & Yao, Y. (2010). Measurement and prediction of water coverage of blade ring in a turbocharger. In Proceedings of the Sixth International Conference on Computational Fluid Dynamics. https://doi.org/10.1007/978-3-642-17884-9

Simulation of gas-water two-phase flow in diesel turbocharger (2010)
Book Chapter
Yao, J., Yao, Y., Mason, P., Zhang, T., Heyes, F. J., & Roach, P. E. (2010). Simulation of gas-water two-phase flow in diesel turbocharger. In American Institute of Physics Conference Proceedings (723-728)

Numerical study of hole shape effect on blade cooling effectiveness (2010)
Journal Article
Yao, J., Sian, S., Yao, Y., & Davis, T. W. (2010). Numerical study of hole shape effect on blade cooling effectiveness. Modern Physics Letters B, 24(13), 1295-1298. https://doi.org/10.1142/S0217984910023463

Numerical study of hole shape effect on blade adiabatic cooling effectiveness has been carried out on four geometry models comprising a standard cylindrical hole, a cylindrical hole with an upstream ramp, a shaped diffuser, and a double console slot.... Read More about Numerical study of hole shape effect on blade cooling effectiveness.

Thrust prediction in thermally choked ram accelerator (2010)
Presentation / Conference
Bengherbia, T., Yao, Y., Bauer, P., & Knowlen, C. (2010, January). Thrust prediction in thermally choked ram accelerator. Paper presented at AIAA 48th Aerospace Sciences Meeting

Effect of hole shape on blade cooling effectiveness (2010)
Presentation / Conference
Yao, J., Sian, S., Khan, J., & Yao, Y. (2010, January). Effect of hole shape on blade cooling effectiveness. Paper presented at AIAA 48th Aerospace Sciences Meeting

One-dimensional performance modelling of the ram accelerator in sub-detonative regime (2010)
Journal Article
Bengherbia, T., Bauer, P., Yao, Y., & Knowlen, C. (2010). One-dimensional performance modelling of the ram accelerator in sub-detonative regime

A one-dimensional performance analysis code has been developed at the ”Laboratoire de Combustion et de D´etonique” to predict the thrust in the thermally choked ram accelerator propulsive mode. This research code incorporates the following equations... Read More about One-dimensional performance modelling of the ram accelerator in sub-detonative regime.

Equations of state for 1-D modelling of ram accelerator thrust in sub-detonative propulsion mode (2010)
Journal Article
Bengherbia, T., Yao, Y., Bauer, P., & Knowlen, C. (2010). Equations of state for 1-D modelling of ram accelerator thrust in sub-detonative propulsion mode. International Journal of Engineering Systems Modelling and Simulation, 2(3), 154-161. https://doi.org/10.1504/IJESMS.2010.035110

A one-dimentional performance analysis code has been developed at eh Laboratoire de Combustion et de Detonique to predict the thrust in the thermally choked ram accelerator propulsion mode. This code includes the real gas effect in steady calculation... Read More about Equations of state for 1-D modelling of ram accelerator thrust in sub-detonative propulsion mode.

Equations of state for 1-D modelling of ram accelerator thrust in thermally choked propulsion mode (2010)
Journal Article
Bengherbia, T., Yao, Y., Bauer, P., & Knowlen, C. (2010). Equations of state for 1-D modelling of ram accelerator thrust in thermally choked propulsion mode. International Journal of Engineering Systems Modelling and Simulation, 2(3), 154-161. https://doi.org/10.1504/IJESMS.2010.035110

A one-dimensional performance analysis code has been developed at the Laboratoire de Combustion et de Détonique to predict the thrust in the thermally choked ram accelerator propulsion mode. This code includes the real gas effect in steady state calc... Read More about Equations of state for 1-D modelling of ram accelerator thrust in thermally choked propulsion mode.

The effect of variable gas property on axial turbine performance (2010)
Journal Article
Yao, Y., & Amos, I. (2010). The effect of variable gas property on axial turbine performance. International Journal of Engineering Systems Modelling and Simulation, 2(3), 190-198. https://doi.org/10.1504/IJESMS.2010.035115

Industrial gas turbine flow has been evaluated by using computational fluid dynamics with a variable gas property model. The study of a three-stage turbine model has revealed some considerable variable gas property effects on the engine performance.... Read More about The effect of variable gas property on axial turbine performance.

The effect of hole shape on blade cooling effectiveness (2010)
Journal Article
Yao, Y., & Yao, J. (2010). The effect of hole shape on blade cooling effectiveness. International Journal of Engineering Systems Modelling and Simulation, 2(4), 242-248. https://doi.org/10.1504/IJESMS.2010.038144

The high temperature conditions under which turbine blades operate pose a constraint on their service lifetime. One industrial solution is to apply the film cooling and the cooling effectiveness is generally determined by flow conditions, cooling hol... Read More about The effect of hole shape on blade cooling effectiveness.