Computational fluid dynamics simulation and wind tunnel testing on microlight model by Ishak, Iskandar Shah

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Unsteady aerodynamic wake of helicopter main-rotor-hub assembly by Ishak, Iskandar Shah

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Effects of boundary layer scrapper on aerodynamic characteristics for automotive wind tunnel testing by Mohd. Zali, Izzat Azim, Ishak, Iskandar Shah

Computational fluid dynamic studies on helicopter main-rotor-hub assembly unsteady wake by Mat Lazim, Tholudin, Mansor, Shuhaimi, Ishak, Iskandar Shah

Experimental research on helicopter tail shake phenomenon by Ishak, Iskandar Shah, Mansor, Shuhaimi, Mat Lazim, Tholudin

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Wind tunnel tests on a generic eurocopter 350Z helicopter by Ishak, Iskandar Shah, Mat Lazim, Tholudin, Mansor, Shuhaimi

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Numerical studies on turbulence modelling of symmetrical aerofoil by Ishak, Iskandar Shah, Dahalan, Md. Nizam, Othman, Nurain

Static analysis of unsteady aerodynamics wake of simplified helicopter model via simulation work by Othman, Nurain, Ishak, Iskandar Shah, Dahalan, Md. Nizam

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Wind-lens turbine design for low wind speed by Takeyeldein, Mohamed M., Ishak, Iskandar Shah, Mat Lazim, Tholudin

Static analysis of unsteady aerodynamics wake of simplified helicopter model via simulation work. by Othman, Nurain, Ishak, Iskandar Shah, Dahalan, M. D. Nizam

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ICT strategic planning in malaysia public research institute by Ishak, Iskandar Shah, Alias, Rose Alinda, Adam, U., Suradi, Z.

Computational analysis of a generic bell 206b helicopter tail rotor blade using ansys fluent by Ammoo, Mohd. Shariff, Jaswar, Jaswar, Ishak, Iskandar Shah, Mahamad, Firdaus

Wind tunnel test on generic agusta-bell 206b helicopter tail rotor blades by Mahamad, Firdaus, Koto, Jaswar, Ishak, Iskandar Shah, Ammoo, Mohd. Shariff

Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method by Mahamad, Firdaus, Koto, Jaswar, Ishak, Iskandar Shah, Ammoo, Mohd. Shariff

Development of a dynamic wind tunnel rig for aircraft pure pitching motion by Mansor, Shuhaimi, Ishak, Iskandar Shah, Ong, Meng Wei, Fahrurazi, Istas

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Pressure distribution on helicopter fuselage by Aris, Anas Faiz, Ishak, Iskandar Shah, Ali, Airi, Othman, Norazila

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Propeller locations study of a generic delta wing UAV model by Kasim, Khushairi Amri, Mat, Shabudin, Ishak, Iskandar Shah, Mansor, Shuhaimi

Rudimentary effects of emblematic gust excitations on the lift performance of coaxial helicopter rotor blades by Abdul Awal, Ziad, Ammoo, Mohd. Shariff, Mansor, Shuhaimi, Ishak, Iskandar Shah

Review on aerodynamic characteristics of helicopter tail rotor propeller using quasi-continuous vortex lattice method by Firdaus, Firdaus, Koto, Jaswar, Ammoo, Mohd. Shariff, Ishak, Iskandar Shah, Nofrizal, Nofrizal

Design and structural analysis of a quadrotor by Ammoo, Mohd. Shariff, Ishak, Iskandar Shah, Mat, Shabudin, Daud, Mohd. Ehsanul Hafizi