Propeller-Tail Interaction
After the complete sizing and design of the V-tail of the FVA-30, an important effect affecting the tail was studied again in more detail during the last semester: The interaction …
Flight Performance Computer Revision
The overall propulsion design depends significantly on the performance requirements resulting from the planned flight profile. The flight performance computer of the FVA-30 used in the preliminary design was based …
Wing Load Comparison with the e-Genius II
In the last article, a first load comparison between the wings of FVA-30 and e-Genius was carried out. Based on the section loads of the wing determined with our load …
Control Unit & HMI
The system architecture of the FVA-30 is a continuous evolution driven by the requirements of the various components of the aircraft. Important for the design is not only the electrical …
Engine Tests: Approval Regulations and Test Design
To prepare the engine runs for the EMRAX 228 HV used, we followed the certification regulations of JAR 22 (Section H Subsection Test Bench Runs) and then made a proposal …
Cooling Concept for Motor and Inverter
After working out a comprehensive selection of cooling concepts, the choice fell on a conventional concept based on a finned radiator typical of the automotive industry. This essentially guaranteed a …