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pro vyhledávání: '"Manaf Muhammed"'
Autor:
Manaf Muhammed, Muhammad Shakeel Virk
Publikováno v:
Drones, Vol 8, Iss 4, p 148 (2024)
The operational regime of Unmanned Aerial Vehicles (UAVs) is distinguished by the dominance of laminar flow and the flow field is characterized by the appearance of Laminar Separation Bubbles (LSBs). Ice accretion on the leading side of the airfoil l
Externí odkaz:
https://doaj.org/article/f24d0180e2e449ce9daebfc9a2609cb6
Autor:
Manaf Muhammed, Muhammad Shakeel Virk
Publikováno v:
Aerospace, Vol 10, Iss 3, p 261 (2023)
Ice accretion on rotary-wing unmanned aerial vehicles (RWUAVs) needs to be studied separately from the fixed-wing UAVs because of the additional flow complexities induced by the propeller rotation. The aerodynamics of rotatory wings are extremely cha
Externí odkaz:
https://doaj.org/article/6aa011c62add4f49825f8f9f3a56aed5
Autor:
Manaf Muhammed, Muhammad Shakeel Virk
Publikováno v:
Drones, Vol 6, Iss 4, p 86 (2022)
Ice accretion on commercial aircraft operating at high Reynolds numbers has been extensively studied in the literature, but a direct transformation of these results to an Unmanned Aerial Vehicle (UAV) operating at low Reynolds numbers is not straight
Externí odkaz:
https://doaj.org/article/a504ec8fff534017aeb614b94d3c223d