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Publications
Taravat Khadivi
Journal Articles
 
bullet Khadivi T & Savory E, 2013. Experimental and numerical study of flow structures associated with low aspect ratio elliptical cavities. ASME Journal of Fluid Engineering, 135(4), pp. 041104-1-14.
bullet Soltani MR, Khadivi T & Hosseini AA, 2004. Fluid flow study over the wing of a fighter-type aircraft model. International Journal of Engineering, Transcriptions B: Applications, 17(4).

Conference Papers
 
bullet Khadivi T & Savory, E, 2009. Numerical analysis of flow around low aspect ratio cavities with elliptical and rectangular planforms. CFD Society of Canada Conference, 3-5 May, Kanata, Canada.
bullet Khadivi T & Savory, E, 2009. Numerical analysis of flow over low aspect ratio elliptical cavities. Western Research Forum, The University of Western Ontario, February, London, Canada.
bullet Khadivi T & Savory E, 2008. CFD modeling of flow over elliptical cavities with varying depths. Canadian Society for Mechanical Engineering Forum, 5-8 June, Ottawa, Canada.
bullet Naghib Lahouti, A, Nazarinia, M. & Khadivi T, 2003. Investigation of the effects of nose shape of strap-on boosters on aerodynamic characteristics of a launch vehicle. 4th
National Conference of Iranian Aerospace Society
, February, Tehran, Iran.
bullet Soltani MR, Khadivi T & Davari AR, 2002. Flow control over the wing of a fighter-type configuration using boundary layer suction. International Council of the Aeronautical Sciences Congress, September, Toronto, Canada.
bullet Nejat A, Khadivi T & Naghib Lahouti A, 2002. Parametric analysis of aerodynamic characteristics of launch vehicles with strap-on boosters. International Council of the
Aeronautical Sciences Congress
, September, Toronto, Canada.
bullet Soltani MR, Khadivi T & Davari AR, 2002. Flow field study over the wing of a high angle-of-attack research vehicle (HARV) model. 9th Asian Congress of Fluid Mechanics, May, Esfehan, Iran.
bullet Soltani MR & Khadivi T, 2002. Effects of suction on the pressure distribution over the
wing of a highly maneuverable aircraft.10th Annual Conference of Iranian Society of
Mechanical Engineers
, May, Esfehan, Iran.

Academic work
 
bullet Khadivi T 2012. Numerical study of flow structures associated with low aspect ratio elliptical  cavities. PhD Thesis, University of Western Ontario, London, Ontario, Canada.
bullet Khadivi T, 2001. Effects of roughness and suction on the pressure distribution over the
wing of a highly maneuverable aircraft. MSc Thesis, Sharif University of Technology, Tehran, Iran.
bullet Khadivi T, 1999. Aerodynamic calculations of a foil craft. BSc Thesis, Sharif University of Technology, Tehran, Iran.


2004 launch, afm/c.dybenko; 2004-2005 maintenance, j.dybenko; 2006-2010 maintenance, w.lin; 2010-2012 maintenance, k.elliott; 2012 - webmaster, s.ali; updated July 2014