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Dr. Adnan Maqsood
Associate Professor
Department of Computational Engineering

National University of Sciences and Technology (NUST)
Research Centre of Modelling and Simulation(RCMS), Academic-I Building, NUST Campus, H-12, Islamabad Pakistan
Tel : +92-51-9085-5734

Aerodynamics/Flight Mechanics & Control/Human Factors

PhD (Mechanical & Aerospace Engineering)

Adnan Maqsood is Tenured Associate Professor at Research Centre for Modelling & Simulation, National University of Sciences and Technology (NUST), Pakistan. He received his Bachelor’s degree in Aerospace Engineering from NUST, Pakistan in 2005 and PhD from Nanyang Technological University (NTU), Singapore in 2012. Currently, he is engaged in graduate teaching and research and heading Mechanics Interdisciplinary Group (MIG) ( The current research interests of Dr. Adnan Maqsood are associated with: Unmanned Air Vehicle (UAV) Systems, Flight Dynamics and Control, Nonlinear Dynamics, Applied & Computational Aerodynamics and Human Factors in UAVs. He is successful in securing both industrial and public funding. At NUST, he has effectively managed and participated as principal and co-principal investigator in 09 different research projects funded by Higher Education Commission (HEC), Pakistan Air Force (PAF), Pakistan Aeronautical Complex (PAC) and Pakistan Ordnance Factories (POF) with total funding grant of more than 11 Million PKR. He has authored 53 scientific publications (peer reviewed journal publications and international conference proceedings). He is actively looking after Belt & Road Aerospace Innovation Alliance (BRAIA), founded in 2017, from NUST.

Research Focus Areas:

MIG thematic areas focus on problem-centric solution approach rather than solution-centric problem-search. Working in collaboration, MIG customize methodologies and carry out innovative applied research in the area of aerodynamics, flight mechanics & control. Currently, MIG researchers are actively pursuing following thematic / focus areas:

1.Aerodynamics, Flight Mechanics & Control of Fixed-Wing Small Unmanned Aircraft Systems. 

Small Unmanned Aircraft Systems with the wing span less than one meter have gained significant attention in recent years because of its versatility in multi-faceted mission profiles. Conceptually, these systems should be capable of immediate deployment and operated through a palm sized ground control station by a single operator. Even though this area of research is pretty renowned in academia for the last two decades, however, lot of challenges impedes its large-scale operational deployment.
Typical attributes associated with the aerodynamics of Small Unmanned Aircraft Systems (UAS) are low Reynolds number, low altitude flying environments and low aspect ratio platforms. These attributes give birth to several challenges such as poor aerodynamic performance, nonlinear/complex lift patterns and reduced gust tolerance. Specifically we are working on:
  • Configuration Aerodynamics: We are exploring biplanes, flexible membrane wings and different morphing configurations to enhance aerodynamic performance in this flight regime.
  • Utilization of Polhamus method to segregate potential & vortex lift associated with these platforms and generate an alternate way of assessing aerodynamic contributions.
  • Engineering the nature-inspired corrugation for small UAS platforms.

Similarly, the attributes associated with the flight mechanics and control for these systems are expanded flight envelopes, low moment of inertia and small stability margins with high design versatility. These attributes give birth to the several challenges out of which a few are: triggering of nonlinear phenomena, dynamic stability estimation and flight performance prediction. We are currently working on following approaches to build new knowledge in this area: 

  • Evaluation of dynamic stability derivatives using CFD. Our major focus is tilted towards studying the effect of geometric variables on dynamic damping behavior.
  • Different optimization algorithms are used to study versatile trajectories associated with small UAS such as: transitions between hover & cruise, perching & dynamic soaring maneuvers. One of our recent initiatives is the characterization of perching maneuvers performed by flying insects.
  • Development of surrogate models to evaluate the performance & find underlying scalability trends between geometric & performance parameters.

2. Limit Cycle Oscillations in Aerospace Systems: 

Limit Cycles are self-sustained oscillations manifested by dynamic systems that are mostly undesirable in aerospace applications. Linear systems theory is limited and cannot decipher the limit cycle characteristics in relation to the aircraft parameters. To overcome this limitation, nonlinear analysis is required.


Complex dynamic systems generally exhibit a mixture of fast and slow response. Some parameters of a certain system may govern the fast dynamic behavior while other may affect the slow dynamic response of the system. In order to fully understand the system so that desired alterations during design and development cycle can be made, understanding the response due to relevant parameters on the slow and fast system behavior can be vital. Generally, instabilities in slow behavior are less threatening than in the fast dynamics. The Multiple Time Scales (MTS) approach separates these slow and fast manifolds of the system explicitly and is based exactly on this separation idea. The idea of the extension is to transform the existing dimension of time to a multiple dimensional space. Since many physical systems of interest exhibit multiple natural time scales, the MTS method is applicable to a wide range of problems. One example is the separation of phugoid mode (slow varying manifold) and short-period mode (fast varying manifold) in aircraft longitudinal dynamics.


Currently, we are working on following problems:

  • Effect of low-aspect ratio rectangular wings on wing-rock.
  • Effect of compressor characteristic curve on surge in axial flow compressors.
  • LCO of Atmospheric Entry Vehicles in low supersonic regime.
  • Pressure Oscillations inside Combustion Chamber of solid rocket motors.

3.Aerodynamics & Flight Mechanics of Supersonic Blunt Bodies with Active / Passive Flow Control. 

The main scientific aim of this project is to reduce and modify the nose shock wave in order to generate smaller drag force and / or better conditions to overcome sonic barrier and to diminish sonic boom intensity. 

The main motivation of this project is to understand the complex shock wave pattern formed by the nose of the aircraft and alleviate its adverse contributions that are high drag, high acoustic signature and high aerodynamic heating.Specifically, feasibility of different passive, active and hybrid flow control techniques to tailor the shock wave characteristics are currently investigated. In near future, effect of active flow control techniques on static and dynamic stability characteristics will also be investigated.

The research in this area is pursued through active collaboration with Dr. Laurent Dala, Northumbria University, UK.


4.Design & Development of Energy-Efficient Electric Fan Blades 

This research pertains to the improvement in the energy efficiency of pedestal and ceiling fans through aerodynamic design refinement of blades. The fan industry of Pakistan is renowned at national and international levels. This is widely considered as an elite sector that is fulfilling national needs of domestic electric fans as well as exporting their products. Gujrat, a hub of fan industry hosts about 300 Small and Medium Enterprises (SMEs). These SMEs are facing tough competition because of advancement in technology, requirement of energy efficiency and failure to comply national / global quality standards. As a result, different fan manufacturers are approaching scientific experts in academia to improve their product design. In this research, we will be collaborating with STARCO® Fans, Gujrat, an industry that has evolved during the last 10 years from a small setup to a substantially large enterprise with primary focus on ceiling, pedestal and wall-mounted fan manufacturing. MIG has already executed a small-scale project with STARCO® Fans in the past in which one ceiling fan blade design of one product was optimized. National University of Sciences & Technology (NUST) and STARCO® Fans intend to expand the scope of collaboration. In this research, aerodynamics body of knowledge is used to refine / redesign / optimize the pedestal and ceiling fan blade designs through computational and experimental approaches. The results produced through this research are lucrative in the sense that implementation cost of the solutions can boost the quality of products with zero investment cost. Moreover, the proposed solutions do not require any improvisation in existing production line.


(Google Scholar ID :


  • Mir, I.; Maqsood, A.; Akhtar, S.; and Eisa, S. A. (2019). Guidance and control of standoff air-to-surface carrier vehicle. The Aeronautical Journal. 123(1261), 283-309. (Impact Factor ~ 0.696)
  • Mir, I.; Taha, H.; Eisa, S. A. and Maqsood, A. (2018). A controllability perspective of dynamic soaring. Nonlinear Dynamics. 2018, 1-16. (Impact Factor ~ 4.339)
  • Mir, I.; Eisa, S. A. and Maqsood, A. (2018). Review of dynamic soaring: technical aspects, nonlinear modeling perspectives and future directions. Nonlinear Dynamics. 2018, 1-28. (Impact Factor ~ 4.339)
  • Mir, I.; Maqsood, A.; and Akhtar, S. (2018). Biologically Inspired Dynamic Soaring Maneuvers for an Unmanned Air Vehicle Capable of Sweep Morphing. International Journal of Aeronautical and Space Sciences. 19(4), 1006-1016. (Impact Factor ~ 0.45)
  • Usman, M., Maqsood, A., Mulkana, S. R. and Riaz, R. (2018). Gap Effect on Flight Performance and Longitudinal Stability of Biplane Micro Air Vehicles. International Journal of Mechanical Engineering and Robotics Research. 7 (6), 635-642. (Scopus indexed)
  • Adeeb, E., Sohn, C. H.,  Maqsood, A. and Afaq, M. A. (2018). Design Optimization of Ceiling Fan Blades with Nonlinear Sweep Profile. Journal of Applied Fluid Mechanics. 11(5), 1153-1162. (Impact Factor ~ 1.09)
  • Alam, M. and Maqsood, A. (2018). Conceptualization of Corporate Setup of an Aviation Engineering Complex through Systems Engineering Process. International Journal of Science and Engineering Investigations. 7 (79), 110-114. (Google Scholar indexed)
  • Mir, I.; Maqsood, A.; Eisa, S. A.; Taha, H.; and Akhtar, S. (2018). Optimal Morphing – Augmented Dynamic Soaring maneuvers for Unmanned Air Vehicle Capable of Span and Sweep Morphologies. Aerospace Science & Technology. 79(2018), 17-36. (Impact Factor ~ 2.228)
  • Ahmed, W., Maqsood, A., and Riaz, R. (2018). Multiple Time Scale Analysis of Pressure Oscillations in Solid Rocket Motors. Results in Physics. 8(2018), 1068-1075. (Impact Factor ~ 2.147)
  • Nasim, A., Maqsood, A. and Saeed, T. (2017). Multicore and GPU based Pupillometry using Parabolic and Elliptic Hough Transform. International Journal of Mechanical Engineering and Robotics Research. 6 (5), 425-433. (Scopus indexed)
  • Munawar, H. S., Maqsood, A. and Mustansar, Z. (2017). Isotropic Surround Suppression and Hough Transform based Target Recognition from Aerial Images. International Journal of Advanced & Applied Sciences. 4(8), 37-42. (ISI Master List)
  • Bibi, A., Maqsood, A., Sherbaz, S., and Dala, L. (2017). Drag Reduction of Supersonic Blunt Bodies using Opposing Jet & Nozzle Geometric Variations. Aerospace Science & Technology. 69(2017), 244-256. (Impact Factor ~ 2.228)
  • Afaq, M. A., Maqsood, A., Butt, S. I., Tauqeer, T. and Hasan, A. (2017). Aerodynamic Investigation and Redeisgn of Ceiling Fan Blades for Enhanced Energy Efficiency. MAEJO International Journal of Science & Technology. 11(2), 97-114. (Impact Factor ~ 0.469)
  • Siddiqui, M. A., Butt, S. I., Gilani, O., Jamil, M., Maqsood, A. and Zhang, F. (2017). Optimizing Availability of a Framework in Series Configuration Utilizing Markov Model and Monte Carlo Simulation Techniques. Symmetry. 9(7), 01-14. (Impact Factor ~ 1.256)
  • Dawood, A. B., Butt, S. I., Ghulam, H., Siddiqui, M. A., Maqsood, A. and Zhang, F. (2017). Thermal Model of Rotary Friction Welding for Similar and Dissimilar Metals. Metals. 7(6), 01-14. (Impact Factor ~1.704)
  • Rashid, K., Ahmad, R., Maqsood, A. and Mazhar, F. (2016). Knowledge-Based Aerodynamic Estimation of Airships. International Journal of Mechanical Engineering and Robotics Research. 5(4), 239-245. (Scopus indexed)
  • Ramzan, M. and Maqsood, A. (2016). Dynamic Modeling & Analysis of a High Pressure Regulator. Mathematical Problems in Engineering. 2016. (Impact Factor ~ 0.802)
  • Adeeb, E., Maqsood, A., Mushtaq, A. and Sohn, C. H. (2016). Parametric Study and Optimization of Ceiling Fan Blades for Improved Aerodynamic Performance. Journal of Applied Fluid Mechanics. 9(6), 2905-2916. (Impact Factor ~ 0.888)
  • Manzoor, M., Maqsood, A. and Hasan, A. (2016). Quadratic Optimal Control of Aerodynamic Vectored UAV at High Angle of Attack. International Review of Aerospace Engineering. 9(3), 70-79. (Scopus indexed)
  • Sherbaz, S., Maqsood, A. and Khan, J. (2015). Machinery Options for Green Ship. Journal of Engineering Science & Technology Review. 8(3), 169-173. (Scopus indexed)
  • Bibi, A., Maqsood, A. and Go, T. H. (2015). Review on Analysis & Modeling of Dynamic Stability Characteristics of Atmospheric Entry Vehicles. NUST Journal of Engineering Sciences. 7(1), 15-21. (HEC indexed)
  • Go, T. H. and Maqsood, A. (2015). Effect of Aspect Ratio on Wing Rock at Low Reynolds Number. Aerospace Science and Technology. 42, 267-273. (Impact Factor ~ 1.751)
  • Maqsood, A. and Go, T. H. (2015). Aerodynamic Characteristics of a Flexible Membrane Micro Air Vehicle. Aircraft Engineering & Aerospace Technology. 87(1), 30-37. (Impact Factor ~ 0.474)
  • Maqsood, A. and Go, T. H. (2013). Parametric Studies and Performance Analysis of a Biplane Micro Air Vehicle. International Journal of Aeronautical & Space Sciences. 14(3), 229-236. (ISI Masterlist & Scopus indexed)
  • Maqsood, A. and Go, T. H. (2013). Lift Estimation of Low Aspect Ratio Annular Wings Based on Suction Analogy. AIAA Journal. 51(2), 529-534. (Impact Factor ~ 1.165)
  •  Maqsood, A. and Go, T. H. (2012). Optimization of Transition Maneuvers through Aerodynamic Vectoring. Aerospace Science and Technology. 23(1), 363-371. (Impact Factor ~ 0.873)
  • Maqsood, A., Huei, F. H. and Go, T. H. (2012). Propeller Induced Effects on the Aerodynamics of a Small Unmanned-Aerial-Vehicle. Journal of Aerospace Technology and Management, 4(4), 475-480. (ISI Master List & Scopus indexed)
  • Maqsood, A. and Go, T. H. (2012). Design Improvement of a Versatile Ducted-Fan UAV. Journal of Mechanical Engineering, 9(1), 01-17. (Scopus indexed)
  • Maqsood, A. and Go, T. H. (2012). Multiple Time Scales Analysis of Aircraft Longitudinal Dynamics with Aerodynamic Vectoring. Nonlinear Dynamics, 69(3), 731-742. (Impact Factor ~ 3.0)
  • Maqsood, A. and Go, T. H. (2010). Longitudinal Flight Dynamic Analysis of an Agile UAV. Aircraft Engineering & Aerospace Technology, 82(5), 288-295. (Impact Factor ~ 0.372)
  • Maqsood, A. and Go, T. H. (2010). Optimization of Hover-to-Cruise Transition Maneuver Using Variable-Incidence Wing. AIAA Journal of Aircraft, 47(3), 1060-1064.  (Impact Factor ~ 0.552)
  • Conferences:

    • Mir, I, Maqsood, A. and Taha, H. E. and Eisa, S. A. (2019). Soaring Energetics for a Nature Inspired Unmanned Aerial Vehicle. AIAA Scitech 2019 Forum, California, USA. (AIAA 2019-1622)
    • Mir, I, Maqsood, A. and Akhtar, S. (2017). Dynamic Modeling & Stability Analysis of a Generic UAV in Glide Phase. 2017 International Conference on Mechanical, Material and Aerospace Engineering, China. (DOI: 10.1051/matecconf/201711401007)
    • Mir, I, Maqsood, A. and Akhtar, S. (2017). Optimization of Dynamic Soaring Maneuvers to Enhance Endurance of a Versatile UAV. IOP Conference Series: International Conference on Aerospace, Mechanical & Mechatronic Engineering, Thailand. (doi:10.1088/1757-899X/211/1/012010)
    • Mir, I, Maqsood, A. and Akhtar, S. (2017). Optimization of Dynamic Soaring Maneuvrs for a Morphing Capable UAV. AIAA Information Systems-AIAA Infotech @ Aerospace, Grapevine, Texas, USA. (AIAA 2017-0678)
    • Bibi, A., Hussain, Z., Khan, F. and Maqsood, A. (2017). Quantitative Evaluation of Security and Privacy Perceptions in Online Social Networks: A Case Study. 14th International Bhurban Conference on Applied Sciences and Technology, Islamabad, Pakistan.
    • Mumtaz, S., Maqsood, A. and Sherbaz, S. (2016). Computational Modeling of Dynamic Stability Derivatives for Generic Airfoils. 3rd International Conference on Mechanical & Manufacturing Engineering, China.
    • Adeeb, E., Maqsood, A. and Musthaq, A. (2015). Effect of Number of Blades on Performance of Ceiling Fans. 4th International Conference on Advances in Mechanics Engineering, Spain.
    • Adeeb, E., Maqsood, A., Musthaq, A. and Hussain, Z. (2015). Shape Optimization of Non-linear Swept Ceiling Fan Blades through RANS simulations and Response Surface Methods. 12th International Bhurban Conference on Applied Sciences and Technology, Islamabad, Pakistan.
    • Ahmad, S., Ahmad, R. and Maqsood, A. (2014). Parametric Screening and Design Refinement of Ceiling Fan Blades. International Conference on Manufacturing & Engineering Technology (ICMET), China. Pages: 591-595; CRC Press 2014.
    • Afaq, M. A., Maqsood, A., Parvez K. and Mushtaq, A.  (2014). Study on the Design Improvement of an Indoor Ceiling Fan. 11th International Bhurban Conference on Applied Sciences and Technology, Islamabad, Pakistan.
    • Maqsood, A., (2013) Modeling & Simulation: A Methodology to Accelerate Research Endeavors of Pakistan. 1st Kinnaird Multidisciplinary Research Conference, Lahore, Pakistan.
    • Maqsood, A., Chang, W. T. and Go, T. H. (2012). Experimental Investigation of a Biplane Micro Air Vehicle. 28th International Congress of the Aeronautical Sciences, Brisbane, Australia.
    • Maqsood, A., Zeng, Z. and Go, T. H. (2012). Flexible Wing Aerodynamics at Low Reynolds Numbers. 28th International Congress of the Aeronautical Sciences, Brisbane, Australia.
    • Maqsood, A. and Go, T. H. (2012). Optimal Transition Maneuver Stability and Control Using Aerodynamic Vectoring. 50th AIAA Aerospace Sciences Meeting and Exhibit, Nashville, Tennessee, USA. (AIAA 2012-855)
    • Maqsood, A. and Go, T. H. (2011). Transition Maneuver of a Small Unmanned Air Vehicle Using Aerodynamic Vectoring. IEEE Defence, Science and Research Conference, Singapore. (doi: 10.1109/DSR.2011.6026831)
    • Maqsood, A. and Go, T. H. (2010). Transition Flight Analysis of an Agile Unmanned Air Vehicle. 27th International Congress of the Aeronautical Sciences, Nice, France.
    • Maqsood, A., Tan, Y. X. and Go, T. H. (2010). Study on Control Effectiveness of a Ducted-Fan UAV. 27th International Congress of the Aeronautical Sciences, Nice, France.
    • Maqsood, A. and Go T. H. (2009). Study on Aerodynamic-Assisted Transition Control Technique for Versatile UAV. 47th AIAA Aerospace Sciences Meeting and Exhibit, Orlando, Florida, USA. (AIAA 2009-60)
    • Maqsood, A., Masud, J. and Mehdi, A. (2007). Aerodynamic Evaluation of Wing-Strake Modification by Higher-Order Panel Method. 45th AIAA Aerospace Sciences Meeting and Exhibit, Orlando, Florida, USA. (AIAA 2007-677)
    • Akram, F., Masud, J., Rehman, A. and Maqsood, A. (2007). Optimization and Integration of NACA Submerged Inlet For Unmanned Aerial Vehicle Operating in High Subsonic Regime. 5th International Bhurban Conference on Applied Sciences and Technology, Islamabad, Pakistan.
    • Maqsood, A., Masud, J. and Qazi, O. A. (2006) Analysis of Aerodynamic Characteristics of Original and Modified Wing-Strake Arrangement of JF-17 THUNDER Aircraft. 10th National Aeronautical Conference, Risalpur, Pakistan.
    • Mehdi, A., Masud, J., Maqsood, A. and Sheikh, S. R. (2006) Evaluation of Aerodynamic Effect of Upgrade Antenna Modification on DA-20 Aircraft using Linearized Potential Flow Approximation. 10th National Aeronautical Conference, Risalpur, Pakistan.
    • Khwaja, H. A., Maqsood, A., Haq, I., Masud, J. and Sheikh, S. R. (2006) Statistical Evaluation of the Performance Parameters of Dual Working Propulsion Systems in Conjunction by Varying Mass Flow Rate . 10th National Aeronautical Conference, Risalpur, Pakistan.

    Keynote/Invited Speaker:

  • Maqsood, A., (2019) Mechanics Interdisciplinary Group : Aerodynamics & Flight Dynamics Related Research Endeavors. Research Seminar, School of Natural Sciences, NUST, Pakistan.
  • Maqsood, A., (2017) Small Unmanned Aircraft Systems : Aerodynamics, Flight Mechanics & Control. Young Scholars Workshop, Belt & Road Aerospace Innovation Alliance, Qingdao, China.
  • Maqsood, A., (2014) Modeling & Simulation: Science for Youth of Pakistan. Punjab Youth Summit, Lahore, Pakistan.
  • Maqsood, A. (2013). Overview of Low Reynolds Number Flight – On Earth & Mars. 2nd National Conference on Space Sciences, Karachi, Pakistan.

     Post-Graduate Students Supervision/Co-Supervision:

                 Student                  Degree Program
                                          ( Year of Completion)                     Title of Research Thesis
  • Mishma Akhtar  " PhD CS&E (Ongoing) "   Trajectory Optimization of Agile Maneuvers using Deep Reinforcement Learning
  • Shagufta Yasir   " PhD CS&E (Ongoing) "   Aerodynamic & Flight Stability Characteristics of Opposing Jets in Supersonic Flight Regime
  • Imran Mir    " PhD CS&E (2018) "   Dynamics, Numerical Optimization and Control of Dynamic Soaring Maneuvers for a Versatile Unmanned Air Vehicle
  • Muhammad Hamza Naeem   " MS CS&E (Ongoing) "   Numerical Investigation of Limit Cycle Oscillations of Atmospheric Entry Vehicles in Low Supersonic Regime
  • Hamood-ur-Rehman   " MS CS&E (Ongoing) "   Stability Considerations of High-lift Devices
  • Fahad Nawaz    " MS CS&E (Ongoing) "  Aerodynamic Assessment of Generic Airfoil with Active Flow Control
  • Aamir Sultan   " MS CS&E (Ongoing) "   Numerical Investigation of Wing-Rock Phenomenon of Low Aspect Ratio Rectangular Wings at Low Reynolds Number
  • Huzaifa Saeed   " MS CS&E (Ongoing) "   Effect of Corrugation on Dynamic Stability of Dragonfly airfoil
  • Mishma Akhtar   " MS SYSE (2018)  "  Two Dimensional Flight Trajectory Tracking and Analysis of Pterygota
  • Murtaza Alam    " MS SYSE (2018) "    Development of Corporate Framework for Aviation Engineering Complex
  • Muhammad Umair   " MS SYSE (2018) "   Development of Technical Facility Layout for Aviation Engineering Setup
  • Shakeel Awan   " MS SYSE (2017) "   Modeling and Performance Estimation of Formation Flight
  •  Tashfeen Javad   " MS SYSE (2017) "   Development of Surrogate Models for Aircraft Performance Estimation
  • Muhammad Umar   " MS CS&E (2017) "   Flight Dynamic Analysis of Versatile Morphing Capabilities for UAV Applications.
  • Adnan Ashraf   " MS SYSE (2017) "    Modeling of Scalability Laws for Unmanned Air Vehicles
  • Zunera Zahid   " MS SYSE (2017) "   Moodle Authenticator: Proposed Security Enhancement for Learning Management System at NUST
  • Asma Bibi     " MS SYSE (2016) "    Evaluation of Security and Privacy Perceptions in Online Social Networks
  • Waqas Ahmed   " MS CS&E (2016) "    Multiple Time Scale Analysis of Pressure Oscillations in Combustion Chambers
  • Suliman Munawar   " MS CS&E (2016) "   Automatic Detection and Rule Based Verification of Strategic Targets from Multispectral Aerial Images
  • Atiqa Bibi    " MS CS&E (2016) "    Drag Reduction in Supersonic Blunt Bodies Using Opposing Jets
  • Muhammad Usman   " MS CS&E (2016) "    Flight Performance and Longitudinal Stability of Biplane MAVs under Gap Variation
  • Muhammad Ramzan   " MS CS&E (2015) "   Modeling and Simulation of Generic Pressure Regulators
  • Saad Shahzad Sultan   " MS CS&E (2015) "    Nonlinear Flight Dynamic Analysis of Blunt Body Entry Vehicles Using Multiple Time Scales Method
  • Saleem Mumtaz    " MS CS&E (2015) "   Computational Modeling & Analysis of Pitch Damping Derivatives for Generic Airfoils at Low Reynolds Number
  • Amnah Nasim    " MS CS&E (2014) "    Detection and Cognitive Assessment of Pupil Dilation Using High Performance Computing
  • Kamran Khan Tareen    " MS CS&E (2014) "   Analysis of Surge Phenomena in Axial Flow Compressors
  • Mubashra Manzoor   " MS CS&E (2014) "   Control Synthesis for High Angle of Flight of an Unmanned Air Vehicle Using Aerodynamic Vectoring
  • Ehsan Adeeb   " MS CS&E (2014) "   Computational Analysis of Forward Sweep Effect on Ceiling Fan Blades
  • Shamraiz Ahmed   " MS CS&E (2014) "    Design Optimization of Ceiling Fan Blades using Design of Experiments & Response Surface Methods
  • Aaqib Afaq   " MS CS&E (2013) "   Aerodynamic Design & Optimization of Energy Efficient Ceiling Fan
  • Arooj Fatima   " MS CS&E (2013) "   Numerical Investigation of the Effect of Gap on Biplane Wings for MAV Applications


    Research Staff Supervision:

                     Name                Position                   Association
    • Fahad Nawaz         Research Associate    2019-Ongoing
    • Huzaifa Saeed        Research Associate    2019-Ongoing
    • Shoaib Sultan         Research Assistant    2019-Ongoing
    • Waleed Khalid        Research Associate    2018
    • Muhammad Umar  Research Associate    2018-Ongoing
    • Jawad Zakir            Research Scientist    2018
    • Hassan Naseer        Research Scientist    2018
    • Syed Mohsin           Research Scientist    2018
    • Waseeq Siddiqui     Research Scientist    2018
    • Amnah Nasim         Research Internee    2014
    • Ehsan Adeeb         Research Assistant    2014
    • Aaqib Afaq             Research Assistant    2013-14

  • CSE-901 Advanced Compressible Fluids
  • CSE-902 Advanced Incompressible Fluids
  • CSE-911 Advanced Flight Mechanics
  • SYSE-812 Human Factors Engineering
  • SYSE-821 Unmanned Aircraft Systems
  • SYSE-822 Applied Aerodynamics
  • ME-831 Nonlinear Dynamics