Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition

Summary

Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition is a doctoral thesis^[1].

Key Facts

• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition authored Nay Lin Oo^[2].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's instance of is recorded as doctoral thesis^[3].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's publisher is recorded as ResearchSpace@Auckland^[4].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's copyright license is recorded as Creative Commons Attribution-NonCommercial-ShareAlike 3.0 New Zealand^[5].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's country of origin is recorded as New Zealand^[6].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's publication date is recorded as +2020-00-00T00:00:00Z^[7].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's main subject is recorded as mechanical engineering^[8].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's work available at URL is recorded as https://researchspace.auckland.ac.nz/handle/2292/54572^[9].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's Handle ID is recorded as 2292/54572^[10].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's title is recorded as Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition^[11].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's copyright holder is recorded as Nay Lin Oo^[12].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's thesis submitted to is recorded as University of Auckland^[13].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's on focus list of Wikimedia project is recorded as NZThesisProject^[14].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's copyright status is recorded as copyrighted^[15].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's online access status is recorded as open access^[16].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's thesis committee member is recorded as Rajnish Sharma^[17].
• Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's thesis committee member is recorded as Peter J Richards^[18].

Body

Designation and Status

Low Reynolds Number Aerodynamics of an UAV Wing under Icing Condition's instance of is recorded as doctoral thesis^[3].