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Conceptual Design Tool to Analyze Electrochemically-Powered Micro Air Vehicles

by Douglas J. Pederson

Looky Rating System: Violence 0/5, Love & Romance 0/5, Mental Health 0/5, Language 0/5, Substance Use 0/5, Fear / Horror 0/5, Fantasy / Supernatural 0/5, LGBTQ+ Representation 0/5.

Description

A multi-fidelity conceptual design tool was developed to assess electrochemically-powered micro air vehicles(MAVs). The tool utilizes four areas of contributing analyses (CAs): aerodynamics, propulsion, power management, and power sources to determine the endurance duration of a given mission. The low-fidelity aerodynamic CA consisted of drag polar calculations and the high-level CA used a vortex theory code called Athena Vortex Lattice (AVL).