Ramin Kamali Moghadam

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Assistant Professor

Ph.D.   in  Aerospace Engineering Sharif University of Technology, Tehran, Iran

Dissertation: 

 

M.Sc. in Aerospace Engineering Sharif University of Technology, Tehran, Iran

Thesis: 

 

B.Sc. in  Mechanical Engineering Iran University of Science and Technology, Tehran, Iran

Senior project: 

 

Google scholar address

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Web Site Address: http://ari.ac.ir/kamali

 


Research Interests 

 - CFD

 - Heat Transfer

 - Turbulent Flows

 - Rarefied Gas Dynamics

 - Micro/Nano Scales Flows

 - Dynamic Stability

 - Experimental Aerodynamics

 

 

Publications

 Journal Papers:

1. Zakeri, R., Kamali-Moghadam R. and Mani, M. “New Chemical-DSMC Method in Numerical Simulation of Axisymmetric Rarefied Reactive Flow”, accepted in Physics of Fluid, March 2017.

2. Kamali-Moghadam R. and Solgi, E. “Development of the DSMC Algorithm in Adaptive Cartesian Grid for Simulation of Rarefied Gas flow around 2D Complex Geometries”, accepted in Amirkabir Mechanical Engineering Technology Journal, March. 2017.

3. Kamali-Moghadam R., “Assessment of the URANS algorithm in unsteady turbulence modeling of a jet in cross flow”, accepted in Aerospace knowledge and technology journal, March 2017.

4. Zakeri, R., Kamali-Moghadam R. and Mani, M. “A New Approach for Chemical Reaction Simulation of Rarefied Gas flow by DSMC Method”, Journal of Computer and fluid, 140, 111-121, 2016.

5. Kamali-Moghadam R., Shakeri M., “Numerical investigation of environmental parameters effect on dynamic stability of a reentry capsule”, Amirkabir Mechanical Engineering Technology Journal, DOI: 10.22060/MEJ.2016.758, Nov. 2016.

6. Kamali-Moghadam R., Javadi, Kh. and Kiani, F., “Assessment of the LES & DES turbulence models in simulation of the flow structures around the finite circular cylinder”, Journal of Applied Fluid Mechanics, Vol. 9, No. 2, pp. 909-923, 2016.

7. Kamali-Moghadam R. and Salimi, M.R., “Equilibrium Effects on the Hypersonic Laminar Boundary Layer Flow over Axisymmetric Bodies”, Journal of Space Science and Technology (JSST), Vol. 8, No. 4, pp. 17-25, 2016.

8. Rasi, F. and Kamali-Moghadam R., “Longitudinal Dynamic Derivatives of an Airfoil for Forced Pitching and Plunging motions”, Journal of Modares Mechanical Engineering, Vol. 14, No. 10, pp. 159-166, 2014.

9. Kamali-Moghadam R., Nouri S., Salimi, M.R., Sheida M., Hosseini, A., “Assessment of Boundary Layer and Approximate Equations in Aeroheating of Axisymmetric Vehicles”, Journal of Space Science and Technology (JSST), Vol. 6, No. 3, pp. 39-48, 2013.

10. Hejranfar K. and Kamali-Moghadam R., “Preconditioned Characteristic Boundary Conditions for Solution of the Preconditioned Euler Equations at Low Mach Number Flows”, Journal of Computational Physics, Vol. 231, No. 12, pp. 4384-4402, 2012.

11. Hejranfar K. and Kamali-Moghadam R., “Assessment of Three Preconditioning Schemes for Solution of the Two-Dimensional Euler Equations at Low Mach Number Flows”, International Journal for Numerical Methods in Engineering, Vol. 89, No. 106, pp. 20-52, 2011.

12. Hejranfar K., Esfahanian, V., and Kamali-Moghadam, R., “Dual-code solution procedure for efficient computing equilibrium hypersonic axisymmetric transitional/turbulent flows”, Journal of Aerospace Science & Technology, Vol. 21, No. 1, pp. 64-74, 2012.

13. Hejranfar K. and Kamali-Moghadam R., “A Comparative Study of Two Preconditioners for Solving 3D Inviscid Low Speed Flows”, Applied Mechanics and Materials, Vol. 110-116, pp. 423-430, 2011.

14. Hejranfar K., Kamali-Moghadam, R., “Shock capturing and shock fitting methods for numerical simulation of hypersonic axisymmetric flow around the blunt noses with real gas effects”, Journal of Sharif University of Technology, June 2009.

15. Hejranfar K., Kamali-Moghadam, R. and Esfahanian, V., “Dual-Code Solution Procedure for Efficient Computing Equilibrium Hypersonic Axisymmetric Laminar Flows”, Journal of Aerospace Science & Technology, Vol. 12, No. 2, pp. 135-149, 2008.

 

 Books:

 Book Chapters:

 Conference Papers:

 Kamali-Moghadam, R. and Kahalian, M.J., “Improvement of the IP-DSMC method in temperature prediction of rarefied gas flowfield”, 16th   conference of Iranian aerospace institute, Tehran, Iran, 2017.

2. Kamali-Moghadam, R., “Development of the URANS method in numerical simulation of the nozzle trust vector control using jet in cross flow”, the 25th Iranian International Conference  of Mechanical Engineering, Tehran, Iran, 2017.

3. Kamali-Moghadam, R. and Solgi, E., “Development of the DSMC algorithm for numerical analysis of rarefied gas flow around 2D complex geometries”, the 25th Iranian International Conference  of Mechanical Engineering, Yazd, Iran, 2016.

4. Kamali-Moghadam, R. and Solgi, E., “Using the Cartesian grid for numerical analysis of rarefied gas flow around 2D geometries by the DSMC method”, 16th Conference on Fluid Dynamics, fd2015, Kermanshah, Iran, 2015.

5. Zakeri, R., Kamali-Moghadam, R. and Mani, M., “Development of the DSMC algorithm for numerical analysis of rarefied gas flow around 2D complex axisymmetric geometries using body fitted unstructured grid”, 15th conference of Iranian aerospace institute, Tehran, Iran, 2014.  

6. Kamali-Moghadam, R. and Solgi, E., “Using the adaptive Cartesian grid for performance improvement of numerical analysis of rarefied gas flow around 2D complex geometries”, 15th conference of Iranian aerospace institute, Tehran, Iran, 2014.

7. Kamali-Moghadam, R. and Shakeri, M., “Numerical simulation of dynamic stability of a reentry capsule in forced pitching oscillation”, the 23th Iranian International Conference  of Mechanical Engineering, Tehran, Iran, 2014.

8. Kamali-Moghadam, R. and Shakeri, M., “Numerical investigation of environmental parameters effect on dynamic stability of a reentry capsule”, the 23th Iranian International Conference  of Mechanical Engineering, Tehran, Iran, 2014.

9. Kamali-Moghadam, R., Solgi, E. and Zakeri, R., “Assessment of the variable hard sphere model (VHS) and general hard sphere model (GHS) in numerical simulation of rarefied gas flow using the DSMC method”, the 23th Iranian International Conference  of Mechanical Engineering, Tehran, Iran, 2014.   

10. Kamali-Moghadam, R. and Salimi, M.R. “Assessment of Real Gas Effects on Approximate and Boundary Layer Equations for Hypersonic Laminar Flow over Axisymmetric Bodies”, the International Conferences of Mechanical and Aerospace Engineering (ICMAE2013), Spain, Madrid, 2014.

11. Rasi, F. and Kamali-Moghadam, R. “Effect of Reduced Frequency on Longitudinal Oscillatory Derivatives of an Airfoil Based on Wind Tunnel Data”, the International Conferences of Mechanical and Aerospace Engineering (ICMAE2013), Spain, Madrid, 2014.

12. Kamali-Moghadam, R. and Salimi, M.R. “Integral Matrix Procedure for Laminar Boundary Layer Flow over Axisymmetric Bodies with Real Gas Effects”, 15th Conference on Fluid Dynamics, fd2013, Iran, Bandar Abbas, 2014.

13. Rasi, F., and Kamali-Moghadam, R. “Experiment Study of Longitudinal Oscillatory Derivatives of an Airfoil for Forced Pitching and Plunging motions”, 13th conference of Iranian aerospace institute, Tehran, Iran, 2014.

14. Kamali-Moghadam, R., Salimi, M.R., Sheida, M. and Hosseini, A. “3D Solution of Laminar Boundary Layer Flow Using Axisymmetric Analogy for Hypersonic Flow”, 13th conference of Iranian aerospace institute, Tehran, Iran, 2014.

15. Kamali-Moghadam, R., Shakeri, M., and Jozvaziri, M., “Numerical simulation of dynamic stability of a 2D geometry in free oscillation”, 14th conference of Iranian aerospace institute, Tehran, Iran, 2013.

16. Kamali-Moghadam, R. and Salimi, M.R. “Assessment of Turbulent Models in Boundary Layer Solution Using Integral Matrix Method around the Hypersonic Axisymmetric Bodies”, the  12nd conference of Iranian aerospace institute, Tehran, Iran, 2013.

17. Kamali-Moghadam, R. and Salimi, M.R. “Hypersonic Flow Solution over Axisymmetric Reentry Vehicles Using the Laminar Boundary Layer and Integral Matrix Method”, the  1st aerodynamic-hydrodynamic conferences, Tehran, Iran, 2012.

18. Hejranfar K. and Kamali-Moghadam R., “An Implicit Preconditioning Method for Numerical Solution of 2D Inviscid Compressible Flow at Low Mach Number Using Upwind Algorithm”, the 18th Iranian International Conference  of Mechanical Engineering, Tehran, Iran, 2011.

19. Hejranfar K. and Kamali-Moghadam R., “A Preconditioned Euler Flow Solver for Simulation of Helicopter Rotor Flow in Hover”, the 6th ICCFD: International Conference on Computational Fluid Dynamics, St. Petersburg, Russia, 2010.

20. Hejranfar K. and Kamali-Moghadam R., “A Comparative Study of Two Preconditioners for Solving 3D Inviscid Low Speed Flows”, ICMAE: International Conference on Mechanical and Aerospace Engineering, Kuala Lumpur, Malaysia, 2010.

21. Hejranfar K. and Kamali-Moghadam R., “Using a Preconditioning Method for Numerical Solution of 3D Inviscid Compressible Flow at Low Mach Number Using Upwind Algorithm”, the 9th conference of Iranian aerospace institute, Tehran, Iran, 2010. 

22. Hejranfar K. and Kamali-Moghadam R., “Applying the Preconditioning Method to Roe's Upwind Algorithm for Numerical Solution of 2D Inviscid Compressible Flow at Low Mach Number”, the 12nd Fluid Dynamics Conference, Babol, Iran, 2010.

23. Hejranfar K. and Kamali-Moghadam R., “Evaluation of a Preconditioning Method for Solving 2D Inviscid Compressible Flow at Low Mach Number Using Upwind Algorithm and Unstructured Grid”, the 8th conference of Iranian aerospace institute, Isfahan, Iran, 2009.

24. Hejranfar, K., Esfahanian, V. and Kamali-Moghadam, R., “Dual-Code Solution Procedure for Equilibrium Hypersonic Axisymmetric Transition/Turbulent Flows”, ICAS2006, Hamburg, Germany, 2006.

25. Hejranfar, K., Esfahanian, V. and Kamali-Moghadam, R., “Computation of Hypersonic Axisymmetric Flows of Equilibrium Gas over Blunt Bodies”, the 13th Annual Conference on Computational Fluid Dynamics, Canada, 2005.

26. Hejranfar, K., and Kamali-Moghadam, R., “Effect of Shock Boundary Condition on Accuracy of Hypersonic Flowfield with Real Gas Effect”, the 14th Iranian International Conference  of Mechanical Engineering, Isfahan, Iran, 2005.

27. Kiani, H., Kamali-Moghadam, R. and Azimi, A. “Comparison of Effect of Non-Conservative Interpolation Methods in a Multiblock Flowfield on Accuracy of Axisymmetric Viscose Flow”, the 14th Iranian International Conference  of Mechanical Engineering, Isfahan, Iran, 2005.

28. Hejranfar, K., Kamali-Moghadam, R. and Azimi, A. “Using the multiblock method for numerical solution of hypersonic axisymmetric flow with real gas effect”, the 6th conference of Iranian aerospace institute, Tehran, Iran, 2005.

29. Hejranfar, K., Esfahanian, V. and Kamali-Moghadam, R., “Numerical Solution of Hypersonic Axisymmetric Flows over Blunt Noses including Equilibrium Gas Effects”, the 9th Fluid Dynamics Conference, Shiraz, Iran, 2004.

30. ShojaeeFar, M. H., Kamali-Moghadam, R., and Noorpoor, A., “Numerical Analysis on Exhaust Flow around Exhaust Valve”, the ASME-ICED Technical Conference, Salzburg, Austria, 2003.

 

 

Teaching Experiences

 

Viscose Flow in Aerospace Research Institute

Rarefied Gas Flow in Aerospace Research Institute

Turbulent Flow in Aerospace Research Institute

Subsonic Flow in University of Tehran 

Supersonic Flow in University of Tehran

CFD in University of Tehran

Unsteady Flow in Imam Hossein University

 

Research Supervision

  

 

 

Professional Experiences

• Design, test and manufacturing of measurement system of hot gas properties for the MGT-30MD turbine.

• Design, test and manufacturing of thermal management system for a spacecraft.

• Developing a 3D code using DSMC method to investigate aero heating around the blunt bodies in reactive rarefied gas flows.

• Developing a 3D structured multi-block code with URANS turbulence modeling.

• Developing a 3D boundary layer code using integral method to investigate aero heating around the blunt bodies in hypersonic flows. 

• Developing the parallel processing in shared memory structure (OpenMP) in 3D unsteady finite volume solver.

• Investigation of LES and DES turbulence models around the finite circular cylinder.

• Numerical simulation of the trust vector controlling by a pulsing cross jet in nozzle exit using URANS developed code. 

• Calculating and analysis of the unsteady damping coefficients for the 3D geometries by Fluent software for investigation of dynamic stability. 

• Developing a high-order 3D upwind solver by finite-volume technique in rotating frame using unstructured mesh. The developed code has been used for numerical simulating of industrial rotor blades of turbomachines and helicopter. 

• Developing a 2D/3D preconditioning solver for solving low Mach number flows.

• Developing a dual-code solution procedure (TLNS-PNS) for efficient computing equilibrium hypersonic axisymmetric laminar and turbulent flows. 

• Developing a multi-block code with real gas effects for numerical simulation of complex configurations at high speeds. 

• Implementation of the conservative and non-conservative interpolation between the interface of the blocks boundaries for the multi-block code. 

 

 

 

 
 
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