Research

Flow Control, Aerodynamics of Sport Vehicles, Aerodynamics of Sport Vehicles, Boundary Layer Flows, Diagnostics in Flow Measurements

Publications

Publications of specific relevance to

2018

AVITAL E, Korakianitis T and MOTALLEBI F (2018). Low Reynolds number proprotor aerodynamic performance improvement using the continuous surface curvature design approach. Cambridge University Press (Cup)  Aeronautical Journal  vol. 123, (1259) 20-38. 10.1017/aer.2018.124

NAYEBOSSADRI S, AVITAL E, MOTALLEBI F and Kenyon G (2018). NASAL INTERNAL AND EXTERNAL AERODYNAMICS FOR HEALTHY AND BLOCKED CAVITIES. World Scientific Publishing  Journal of Mechanics in Medicine and Biology  vol. 18, (5) 1850050-1850050. 10.1142/S0219519418500501

2009

Zare Shahneh A and 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 and 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

2008

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 and 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

2006

Cohen GS and 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

2004

Dabnichki P, Motallebi F and 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

Motallebi F, Dabnichki P and 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

Dabnichki P, Motallebi F and 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

2002

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  ? 

2001

Rowe A, Fry ALA and 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

2000

Cohen GS, Motallebi F and Horton HP (2000). Some observations on the relaminarisation of a supersonic turbulent boundary layer. Aeronaut J  vol. 104, (1041) 557-559. 10.1017/s0001924000017905

1996

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

1994

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