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
.
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
,