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Publications:  Dr Fariborz Motallebi

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.
10.1017/aer.2018.124
https://qmro.qmul.ac.uk/xmlui/handle/123456789/53103
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,
10.1142/S0219519418500501
https://qmro.qmul.ac.uk/xmlui/handle/123456789/42123
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.
10.1115/1.3086591
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.
10.2514/1.37678
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.
10.1017/S0001924000087790
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.
10.1017/S0001924000002372
Cohen GS, Motallebi F(2006). Sub boundary-layer vortex generators for the control of shock induced separation. AERONAUT J vol. 110, (1106) 215-226.
10.1017/S0001924000001196
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.
10.1243/146442004323085545
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.
10.1243/146442004323085545
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.
10.1243/146442004323085554
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.
10.2514/2.1377
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.
10.1017/s0001924000017905
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,
10.1115/2000-GT-0281
Motallebi F(1996). Reynolds number effects on the prediction of velocity profile in compressible flows. AIAA J vol. 34, (4) 870-873.
10.2514/3.13161
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.
10.1017/s0001924000027287
MOTALLEBI F(1994). MEAN FLOW STUDY OF 2-DIMENSIONAL SUBSONIC TURBULENT BOUNDARY-LAYERS. AIAA J vol. 32, (11) 2153-2161.
10.2514/3.12272
MOTALLEBI F(1994). SKIN FRICTION AND VELOCITY PROFILE FAMILY FOR COMPRESSIBLE TURBULENT BOUNDARY-LAYERS - COMMENT. AIAA J vol. 32, (9) 1938-1938.
10.2514/3.12200
MOTALLEBI F(1994). A REVIEW OF THE HOT-WIRE TECHNIQUE IN 2-D COMPRESSIBLE FLOWS. PROG AEROSP SCI vol. 30, (3) 267-294.
10.1016/0376-0421(94)90005-1
Motallebi F (1988). BASE PRESSURE IN TRANSONIC SPEEDS: A COMPARISON BETWEEN THEORY AND EXPERIMENT. American Society of Mechanical Engineers (Paper).
10.1115/88-gt-132
Motallebi F (1988). Base pressure in transonic speeds a comparison between theory and experiment. Proceedings of the ASME Turbo Expo. vol. 1,
10.1115/88-GT-132
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