Dr Fariborz Motallebi
BSc MEng PhD
Publications
- DIFFERENCES IN THE NON LINEAR PROPAGATION OF CRACKLE AND SCREECH (2024)
DOI: 10.25144/24189 - Airborne Transmission of SARS-CoV-2: The Contrast between Indoors and Outdoors
Fluids (2024)
DOI: 10.3390/fluids9030054 - Investigation of the formation and evolution of over-tip shock waves in the pressure-driven tip leakage flow by time-resolved schlieren visualization
Physics of Fluids
DOI: 10.1063/5.0147216 - Conceptual Design of a UVC-LED Air Purifier to Reduce Airborne Pathogen Transmission—A Feasibility Study
Fluids (2023)
DOI: 10.3390/fluids8040111 - Low Reynolds number proprotor aerodynamic performance improvement using the continuous surface curvature design approach
Aeronautical Journal (2018)
DOI: 10.1017/aer.2018.124 - NASAL INTERNAL AND EXTERNAL AERODYNAMICS FOR HEALTHY AND BLOCKED CAVITIES
Journal of Mechanics in Medicine and Biology (2018)
DOI: 10.1142/S0219519418500501 - Base Pressure on a Blunt Base in Transonic Flow: Some Effects of Base Geometry and Bleed Air (2015)
DOI: 10.1115/82-gt-317 - Flow and Heat Transfer in a Rotating Cavity With a Stationary Stepped Casing (2014)
DOI: 10.1115/2000-gt-0281 - 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
DOI: 10.1115/1.3086591 - Effect of submerged vortex generators on shock-induced separation in transonic flow
Journal of Aircraft
DOI: 10.2514/1.37678 - Introduction to the Queen Mary College 100th anniversary of teaching aeronautics special issue of The Aeronautical Journal
AERONAUT J
DOI: 10.1017/S0001924000087790 - Influence of the height of the vortex generators in the control of shock-induced separation of the boundary layers
Aeronautical Journal
DOI: 10.1017/S0001924000002372 - The effect of base bleed on vortex shedding and base pressure in compressible flow
Journal of Fluid Mechanics (2006)
DOI: 10.1017/s0022112081000748 - Sub boundary-layer vortex generators for the control of shock induced separation
AERONAUT J
DOI: 10.1017/S0001924000001196 - 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
DOI: 10.1243/146442004323085545 - Advanced bobsleigh design. Part 1: body protection, injury prevention and performance improvement
P I MECH ENG L-J MAT
DOI: 10.1243/146442004323085545 - Advanced bobsleigh design. Part 2: aerodynamic modifications to a two-man bobsleigh
P I MECH ENG L-J MAT
DOI: 10.1243/146442004323085554 - The effect of a tetrahedral vortex generator model on the control of shock-induced boundary layer separationn at supersonic speeds
- Control of shock-induced separation of sub boundary layer vortex generators
- Effect of Rapid Acceleration on Supersonic Turbulent Boundary Layers.
- On the aerodynamics of two man bobsleigh
The Engineering of Sport 4 - Protection versus performance in bobsleigh ergonomic design
The Engineering of Sport 4 - Influence of boundary-layer thickness on base pressure and vortex shedding frequency
AIAA J
DOI: 10.2514/2.1377 - Influence of boundary-layer thickness on base pressure and vortex shedding frequency
AIAA Journal
DOI: 10.2514/3.14799 - Some observations on the relaminarisation of a supersonic turbulent boundary layer
AERONAUT J
DOI: 10.1017/s0001924000017905 - Reynolds number effects on the prediction of velocity profile in compressible flows
AIAA J
DOI: 10.2514/3.13161 - Reynolds number effects on the prediction of mean flow data for adiabatic 2-D compressible boundary layers
AERONAUT J
DOI: 10.1017/s0001924000027287 - MEAN FLOW STUDY OF 2-DIMENSIONAL SUBSONIC TURBULENT BOUNDARY-LAYERS
AIAA J
DOI: 10.2514/3.12272 - SKIN FRICTION AND VELOCITY PROFILE FAMILY FOR COMPRESSIBLE TURBULENT BOUNDARY-LAYERS - COMMENT
AIAA J
DOI: 10.2514/3.12200 - A REVIEW OF THE HOT-WIRE TECHNIQUE IN 2-D COMPRESSIBLE FLOWS
PROG AEROSP SCI
DOI: 10.1016/0376-0421(94)90005-1 - BASE PRESSURE IN TRANSONIC SPEEDS: A COMPARISON BETWEEN THEORY AND EXPERIMENT.
American Society of Mechanical Engineers (Paper)
DOI: 10.1115/88-gt-132 - Base pressure in transonic speeds a comparison between theory and experiment
Proceedings of the ASME Turbo Expo
DOI: 10.1115/88-GT-132 - BASE PRESSURE ON A BLUNT BASE IN TRANSONIC FLOW - SOME EFFECTS OF BASE GEOMETRY AND BLEED AIR.
American Society of Mechanical Engineers (Paper) - DIFFERENCES IN THE NON LINEAR PROPAGATION OF CRACKLE AND SCREECH (2024)
DOI: 10.25144/24189 - Airborne Transmission of SARS-CoV-2: The Contrast between Indoors and Outdoors
Fluids (2024)
DOI: 10.3390/fluids9030054 - Investigation of the formation and evolution of over-tip shock waves in the pressure-driven tip leakage flow by time-resolved schlieren visualization
Physics of Fluids
DOI: 10.1063/5.0147216 - Conceptual Design of a UVC-LED Air Purifier to Reduce Airborne Pathogen Transmission—A Feasibility Study
Fluids (2023)
DOI: 10.3390/fluids8040111 - Low Reynolds number proprotor aerodynamic performance improvement using the continuous surface curvature design approach
Aeronautical Journal (2018)
DOI: 10.1017/aer.2018.124 - NASAL INTERNAL AND EXTERNAL AERODYNAMICS FOR HEALTHY AND BLOCKED CAVITIES
Journal of Mechanics in Medicine and Biology (2018)
DOI: 10.1142/S0219519418500501 - Base Pressure on a Blunt Base in Transonic Flow: Some Effects of Base Geometry and Bleed Air (2015)
DOI: 10.1115/82-gt-317 - Flow and Heat Transfer in a Rotating Cavity With a Stationary Stepped Casing (2014)
DOI: 10.1115/2000-gt-0281 - 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
DOI: 10.1115/1.3086591 - Effect of submerged vortex generators on shock-induced separation in transonic flow
Journal of Aircraft
DOI: 10.2514/1.37678 - Introduction to the Queen Mary College 100th anniversary of teaching aeronautics special issue of The Aeronautical Journal
AERONAUT J
DOI: 10.1017/S0001924000087790 - Influence of the height of the vortex generators in the control of shock-induced separation of the boundary layers
Aeronautical Journal
DOI: 10.1017/S0001924000002372 - The effect of base bleed on vortex shedding and base pressure in compressible flow
Journal of Fluid Mechanics (2006)
DOI: 10.1017/s0022112081000748 - Sub boundary-layer vortex generators for the control of shock induced separation
AERONAUT J
DOI: 10.1017/S0001924000001196 - 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
DOI: 10.1243/146442004323085545 - Advanced bobsleigh design. Part 1: body protection, injury prevention and performance improvement
P I MECH ENG L-J MAT
DOI: 10.1243/146442004323085545 - Advanced bobsleigh design. Part 2: aerodynamic modifications to a two-man bobsleigh
P I MECH ENG L-J MAT
DOI: 10.1243/146442004323085554 - The effect of a tetrahedral vortex generator model on the control of shock-induced boundary layer separationn at supersonic speeds
- Control of shock-induced separation of sub boundary layer vortex generators
- Effect of Rapid Acceleration on Supersonic Turbulent Boundary Layers.
- On the aerodynamics of two man bobsleigh
The Engineering of Sport 4 - Protection versus performance in bobsleigh ergonomic design
The Engineering of Sport 4 - Influence of boundary-layer thickness on base pressure and vortex shedding frequency
AIAA J
DOI: 10.2514/2.1377 - Influence of boundary-layer thickness on base pressure and vortex shedding frequency
AIAA Journal
DOI: 10.2514/3.14799 - Some observations on the relaminarisation of a supersonic turbulent boundary layer
AERONAUT J
DOI: 10.1017/s0001924000017905 - Reynolds number effects on the prediction of velocity profile in compressible flows
AIAA J
DOI: 10.2514/3.13161 - Reynolds number effects on the prediction of mean flow data for adiabatic 2-D compressible boundary layers
AERONAUT J
DOI: 10.1017/s0001924000027287 - MEAN FLOW STUDY OF 2-DIMENSIONAL SUBSONIC TURBULENT BOUNDARY-LAYERS
AIAA J
DOI: 10.2514/3.12272 - SKIN FRICTION AND VELOCITY PROFILE FAMILY FOR COMPRESSIBLE TURBULENT BOUNDARY-LAYERS - COMMENT
AIAA J
DOI: 10.2514/3.12200 - A REVIEW OF THE HOT-WIRE TECHNIQUE IN 2-D COMPRESSIBLE FLOWS
PROG AEROSP SCI
DOI: 10.1016/0376-0421(94)90005-1 - BASE PRESSURE IN TRANSONIC SPEEDS: A COMPARISON BETWEEN THEORY AND EXPERIMENT.
American Society of Mechanical Engineers (Paper)
DOI: 10.1115/88-gt-132 - Base pressure in transonic speeds a comparison between theory and experiment
Proceedings of the ASME Turbo Expo
DOI: 10.1115/88-GT-132 - BASE PRESSURE ON A BLUNT BASE IN TRANSONIC FLOW - SOME EFFECTS OF BASE GEOMETRY AND BLEED AIR.
American Society of Mechanical Engineers (Paper)
