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Research
  1. Queen Mary University of London
  2. Research
  3. Publications

Publications: Dr Fariborz Motallebi

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AVITAL E, Korakianitis T, MOTALLEBI F ( 2018 ) . Low Reynolds number proprotor aerodynamic performance improvement using the continuous surface curvature design approach . Aeronautical Journal vol. 123 , ( 1259 ) 20 - 38 .
NAYEBOSSADRI S, AVITAL E, MOTALLEBI F, Kenyon G ( 2018 ) . NASAL INTERNAL AND EXTERNAL AERODYNAMICS FOR HEALTHY AND BLOCKED CAVITIES . Journal of Mechanics in Medicine and Biology vol. 18 , ( 5 ) Article 1850050 , 1850050 - 1850050 .
Punekar JN, Avital E, Motallebi F, Li X ( 2017 ) . Differences in the non linear propagation of crackle and screech . 24th International Congress on Sound and Vibration, ICSV 2017 .
Zare Shahneh A, Motallebi F ( 2009 ) . An experimental study on the influence of vortex generators on the shock-induced boundary layer separation at M=1.4 . Journal of Applied Mechanics, Transactions ASME vol. 76 , ( 4 ) 1 - 8 .
Shahneh AZ, Motallebi F ( 2009 ) . Effect of submerged vortex generators on shock-induced separation in transonic flow . Journal of Aircraft vol. 46 , ( 3 ) 856 - 863 .
Motallebi F ( 2008 ) . Introduction to the Queen Mary College 100th anniversary of teaching aeronautics special issue of The Aeronautical Journal . AERONAUT J vol. 112 , ( 1133 ) IV - IV .
Cohen GS, Motallebi F ( 2008 ) . Influence of the height of the vortex generators in the control of shock-induced separation of the boundary layers . Aeronautical Journal vol. 112 , ( 1133 ) 415 - 420 .
Cohen GS, Motallebi F ( 2006 ) . Sub boundary-layer vortex generators for the control of shock induced separation . AERONAUT J vol. 110 , ( 1106 ) 215 - 226 .
Dabnichki P, Motallebi F, Avital E ( 2004 ) . Advanced bobsleigh design. Part 1: Body protection, injury prevention and performance improvement . Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications vol. 218 , ( 2 ) 129 - 137 .
Dabnichki P, Motallebi F, Avital E ( 2004 ) . Advanced bobsleigh design. Part 1: body protection, injury prevention and performance improvement . P I MECH ENG L-J MAT vol. 218 , ( L2 ) 129 - 137 .
Motallebi F, Dabnichki P, Luck D ( 2004 ) . Advanced bobsleigh design. Part 2: aerodynamic modifications to a two-man bobsleigh . P I MECH ENG L-J MAT vol. 218 , ( L2 ) 139 - 144 .
MOTALLEBI F, Shahneh AZ ( 2004 ) . The effect of a tetrahedral vortex generator model on the control of shock-induced boundary layer separationn at supersonic speeds . Conference: 1st European Forum on Flow Control, France
MOTALLEBI F, Cohen SG ( 2002 ) . Control of shock-induced separation of sub boundary layer vortex generators . Conference: Proc IUTM Symposium on Unsteady Separated Flows, Toulouse, France
MOTALLEBI F ( 2002 ) . Effect of Rapid Acceleration on Supersonic Turbulent Boundary Layers . Book of Abstracts, The Ninth Asian Congress of Fluid Mechanics. Editors: Shirani, E, Pishevar, A , ?
Avital E, MOTALLEBI F, Dabnichki P ( 2002 ) . On the aerodynamics of two man bobsleigh . The Engineering of Sport 4 . Editors: Ujihashi, S, Haake, SJ , Conference: 4th International Conference on the Engineering of Sport ( Kyoto, Japan ) 346 - 352 .
DABNICHKI PA, Motallebi F, Avital E ( 2002 ) . Protection versus performance in bobsleigh ergonomic design . The Engineering of Sport 4 . Editors: Ujihashi, S, Haake, SJ , Conference: 4th International Conference on the Engineering of Sport ( Kyoto, Japan ) 346 - 352 .
Rowe A, Fry ALA, Motallebi F ( 2001 ) . Influence of boundary-layer thickness on base pressure and vortex shedding frequency . AIAA J vol. 39 , ( 4 ) 754 - 756 .
Cohen GS, Motallebi F, Horton HP ( 2000 ) . Some observations on the relaminarisation of a supersonic turbulent boundary layer . AERONAUT J vol. 104 , ( 1041 ) 557 - 559 .
Jaafar AA, Motallebi F, Wilson M, Owen JM ( 2000 ) . Flow and heat transfer in a rotating cavity with a stationary stepped casing . Proceedings of the ASME Turbo Expo . vol. 3 ,
Motallebi F ( 1996 ) . Reynolds number effects on the prediction of velocity profile in compressible flows . AIAA J vol. 34 , ( 4 ) 870 - 873 .
Motallebi F ( 1996 ) . Reynolds number effects on the prediction of mean flow data for adiabatic 2-D compressible boundary layers . AERONAUT J vol. 100 , ( 992 ) 53 - 59 .
MOTALLEBI F ( 1994 ) . MEAN FLOW STUDY OF 2-DIMENSIONAL SUBSONIC TURBULENT BOUNDARY-LAYERS . AIAA J vol. 32 , ( 11 ) 2153 - 2161 .
MOTALLEBI F ( 1994 ) . SKIN FRICTION AND VELOCITY PROFILE FAMILY FOR COMPRESSIBLE TURBULENT BOUNDARY-LAYERS - COMMENT . AIAA J vol. 32 , ( 9 ) 1938 - 1938 .
MOTALLEBI F ( 1994 ) . A REVIEW OF THE HOT-WIRE TECHNIQUE IN 2-D COMPRESSIBLE FLOWS . PROG AEROSP SCI vol. 30 , ( 3 ) 267 - 294 .
Motallebi F ( 1988 ) . BASE PRESSURE IN TRANSONIC SPEEDS: A COMPARISON BETWEEN THEORY AND EXPERIMENT . American Society of Mechanical Engineers (Paper) .
Motallebi F ( 1988 ) . Base pressure in transonic speeds a comparison between theory and experiment . Proceedings of the ASME Turbo Expo . vol. 1 ,
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