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drag (3) 3
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diesel / compression ignition engines (2) 2
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SAE technical paper series, Volume 2006-01-3644.
With energy conservation and pollutant emission of paramount importance in today's society, it has emphasized the need for aerodynamic drag reduction in the... 
Computational fluid dynamics | Computer simulation | Drag | Aerodynamics | Body structures | Racing vehicles
eJournal
SAE technical paper series, Volume 2008-01-0947.
This study presents a computationally efficient numerical model that accurately predicts complex spray distribution and spray penetration for a direct... 
Diesel / Compression Ignition engines | Computational fluid dynamics | Drag | Mathematical models | Fuel injection | Emissions
eJournal
SAE technical paper series, Volume 2008-01-0289.
A zero dimensional computer code was developed to predict the performance of an spark ignition internal combustion fuel inducted engine. The code can be used... 
Knock | Thermodynamics | Diesel / Compression Ignition engines | Drag | Mathematical models | Racing engines | Simulation and modeling | Spark ignition engines
eJournal
Journal of Propulsion and Power (0748-4658), ISSN 0748-4658, 09/1995, Volume 11, Issue 5, pp. 894 - 898
The KIVA-11 code was modified to allow calculation of the flow fields in a staged gas turbine combustor including the air-blast fuel nozzle. The results... 
Journal Article
AIAA, ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit, 32nd, Lake Buena Vista, FL; UNITED STATES; 1-3 July 1996, ISSN 0146-3705, 07/1996
A numerical study was performed to investigate the 3D flow with liquid spray injection in a rich burn section of a staged combustor concept consisting of an... 
Conference Proceeding
AIAA, ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit, 31st, San Diego, CA; UNITED STATES; 10-12 July 1995, ISSN 0146-3705, 07/1995
A numerical study was performed to investigate the three-dimensional flow with liquid spray injection in a rich burn section of a staged combustor concept. For... 
Conference Proceeding
In Florida Univ., The 1995 NASA-ODU American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program p 95 (SEE N96-24278 08- 80), 07/1995
A quasi-one-dimensional computer code based on a fuel/air cycle analysis was developed to predict the performance of two and four stroke fuel- inducted... 
Conference Proceeding
ASME, International Gas Turbine and Aeroengine Congress and Exposition, The Hague, Netherlands; UNITED STATES; 13-16 June 1994, 06/1994
A numerical study was performed to investigate the chemically reactive flow with liquid spray injection in a staged combustor concept for reducing pollutant... 
Conference Proceeding
Journal of Propulsion and Power, ISSN 0748-4658, 09/1995, Volume 11, Issue 5, pp. 894 - 898
The KIVA-II code was modified to allow calculation of the flowfields in a staged gas turbine combustor including the air-blast fuel nozzle. The results... 
SPEEDS | AEROSPACE ENGINEERING & TECHNOLOGY
Journal Article
ASME, International Gas Turbine and Aeroengine Congress and Exposition, Houston, TX; UNITED STATES; 5-8 June 1995, 06/1995
The present study compares standard helical flat vane performance with a low loss curved vane designed by the author for idle, and cruise conditions both with... 
Conference Proceeding
AIAA, Aerospace Sciences Meeting & Exhibit, 32nd, Reno, NV; UNITED STATES; 10-13 Jan. 1994, ISSN 0146-3705, 01/1994
This study presents the results of a numerical simulation of a single stage axial compressor. The numerical scheme used solves the unsteady... 
Conference Proceeding
AIAA, ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit, 31st, San Diego, CA; UNITED STATES; 10-12 July 1995, ISSN 0146-3705, 07/1995
The present study compares standard helical flat vane performance with a low loss curved vane designed by the author for idle and cruise conditions at three... 
Conference Proceeding
SAE Technical Papers, 2002
Journal Article
ASME, International Gas Turbine and Aeroengine Congress and Exposition, Houston, TX; UNITED STATES; 5-8 June 1995, 06/1995
This study presents the results of numerical simulations of single-stage transonic axial-flow compressors. The numerical scheme used solves the unsteady... 
Conference Proceeding
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