Print Email Facebook Twitter Meteorite aerodynamics during dark flight Title Meteorite aerodynamics during dark flight: An experimental investigation using a subsonic wind tunnel Author Aduru, Sai Saran (TU Delft Aerospace Engineering; TU Delft Astrodynamics & Space Missions) Contributor de Vet, S.J. (mentor) Cazaux, S.M. (graduation committee) Sciacchitano, A. (graduation committee) Degree granting institution Delft University of Technology Programme Aerospace Engineering Date 2022-01-28 Abstract The dark flight of the meteorite in the atmosphere complicates the estimation of the impact point on the Earth’s surface. The irregular shape of the meteorite affects the aerodynamic forces during the dark flight, which can influence the trajectory of the meteorite. This further complicates the meteorite recovery. Limited knowledge of the aerodynamic properties of meteorite is speculated as one of the major reasons for partial recovery of the meteorites. Therefore, this work experimentally investigates the meteorite aerodynamics during dark flight using a subsonic wind tunnel. The drag coefficient, free fall analysis from 10 km altitude and the rotational aspects were studied using a 3D printed meteorite model. Additionally, the results were implemented in a dark flight code to study the influence of these parameters for a hypothetical meteorite fall. This study proved that aerodynamic forces are very crucial in the meteorite dark flight and strongly influences the meteorite trajectory. Subject Broek in WaterlandStrewn fieldOriented flightShape factorRotation To reference this document use: http://resolver.tudelft.nl/uuid:2cb31e05-37d5-4ef9-8d1a-faae7ffbf5e4 Part of collection Student theses Document type master thesis Rights © 2022 Sai Saran Aduru Files PDF MasterThesis_SGVSAduru_5024730.pdf 11.35 MB Close viewer /islandora/object/uuid:2cb31e05-37d5-4ef9-8d1a-faae7ffbf5e4/datastream/OBJ/view