Hydrogen-Powered Ultralight Training Aircraft — A Systems Engineering Approach
Low-Fidelity Static Aeroelastic Analysis for Jig Shape Optimization of a Solar-Powered Hale Aircraft Wing
A Low-Cost Anechoic Chamber for Rotor Aeroacoustics Research: Design and Validation
From Icing to Helipads: CFD-Based Solutions to Contemporary Rotorcraft Challenges
The Evolution of Piston Aircraft Engines: Development, Performance Indicators, and Technological Advancements
Integrating ADS-B Data for Enhanced Airport Noise Modeling and Environmental Management
Información de la revista
20
MNiSW
10
Google Scholar H5-index
24
Google Scholar H5-median