Erwin Sulaeman, Ph.D.
Affiliations: | 2002 | Virginia Polytechnic Institute and State University, Blacksburg, VA, United States |
Area:
Aerospace EngineeringGoogle:
"Erwin Sulaeman"Parents
Sign in to add mentor| Rakesh K. Kapania | grad student | 2002 | Virginia Tech | |
| (Effect of compressive force on aeroelastic stability of a strut -braced wing.) | ||||
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Publications
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| Siddiqui NA, Aldeeb M, Asrar W, et al. (2018) Experimental investigation of a new spiral wingtip International Journal of Aviation, Aeronautics, and Aerospace. 5: 6 |
| Malik K, Asrar W, Sulaeman E. (2018) Low Reynolds Number Numerical Simulation of the Aerodynamic Coefficients of a 3D Wing International Journal of Aviation, Aeronautics, and Aerospace. 5: 8 |
| Aldheeb MA, Asrar W, Sulaeman E, et al. (2018) Aerodynamics of porous airfoils and wings Acta Mechanica. 229: 3915-3933 |
| Siddiqui NA, Asrar W, Sulaeman E. (2017) Literature Review: Biomimetic and Conventional Aircraft Wing Tips International Journal of Aviation, Aeronautics, and Aerospace. 4: 6 |
| ul-Haque A, Asrar W, Omar AA, et al. (2017) Wind tunnel testing of hybrid buoyant aerial vehicle Aircraft Engineering and Aerospace Technology. 89: 99-105 |
| Haque AU, Asrar W, Omar AA, et al. (2017) Effect of diamond shaped strut with cylindrical pitch rod in subsonic wind tunnel testing Measurement. 99: 1-6 |
| Aldheeb MAM, Asrar W, Sulaeman E, et al. (2016) A Review on Aerodynamics of Non-Flapping Bird Wings Journal of Aerospace Technology and Management. 8: 7-17 |
| Hoq SMA, Sulaeman E, Okhunov A. (2016) Error Analysis of Heat Conduction Partial Differential Equations using Galerkin’s Finite Element Method Indian Journal of Science and Technology. 9 |
| Haque AU, Asrar W, Omar AA, et al. (2015) Preliminary aerodynamic and static stability analysis for hybrid buoyant aerial vehicles at low speeds using digital DATCOM Canadian Aeronautics and Space Journal. 61: 51-60 |
| Haque AU, Hafiz NMA, Kashif SM, et al. (2015) Design and fabrication of a winged hybrid airship model for IIUM-LSWT Advanced Materials Research. 1115: 513-516 |