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pro vyhledávání: '"Riyadh Ibraheem Ahmed"'
Autor:
Azmin Shakrine Mohd Rafie, Abd Rahim Abu Talib, Harijono Djojodihardjo, Riyadh Ibraheem Ahmed
Publikováno v:
Aircraft Engineering and Aerospace Technology. 89:231-245
PurposeThe purpose of this paper is to reformulate the governing equations incorporating major variables and parameters for the design a Micro Air Vehicle (MAV), to meet the desired mission and design requirements.Design/methodology/approachMathemati
Publikováno v:
Aerospace Science and Technology. 62:136-147
With the progress and development of Coanda Micro Air Vehicle (MAV) to date, various configurations have been proposed and developed. For the purpose of designing a Micro Air Vehicle (MAV), that could meet the desired mission and design requirements
Autor:
A.B.D. Rahim bin Abu Talib, Riyadh Ibraheem Ahmed, Harijono Djojodihardjo, Mohd Faisal Abd Hamid
Publikováno v:
Applied Mechanics and Materials. 629:139-144
Coandă effect, which has been widely utilized in many engineering applications for circulation control, is here reviewed for the design of Coandă Micro-Air-Vehicles (MAVs). Based on the review, a basic spherical configuration is analyzed to obtain
Publikováno v:
Journal of Physics: Conference Series. 822:012051
Publikováno v:
2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology.
With the progress of solar sail interplanetary travel in the last two decades, various concepts and technologies have been developed. To that end, two means of sailing, Solar Sail and Electric Sail, will be discussed. The capabilities as well as perf
Publikováno v:
2014 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology.
A mathematical model for lift generation on a doughnut-shaped Coanda micro air vehicle is developed and an analysis on the lift generation due to Coanda effect is carried out utilizing basic principles. A degenerate two-dimensional case is also devel
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 157:012002
The paper establishes the basic working relationships among various relevant variables and parameters governing the aerodynamics forces and performance measures of Coanda MAV in hover and translatory motion. With such motivation, capitalizing on the