Next Article in Journal
A Data-Driven Approach to Identify Flight Test Data Suitable to Design Angle of Attack Synthetic Sensor for Flight Control Systems
Next Article in Special Issue
Predicting Rotor Heat Transfer Using the Viscous Blade Element Momentum Theory and Unsteady Vortex Lattice Method
Previous Article in Journal
Parametric Study of Guidance of a 160-mm Projectile Steered with Lateral Thrusters
Previous Article in Special Issue
Numerical and Experimental Investigation of the Design of a Piezoelectric De-Icing System for Small Rotorcraft Part 3/3: Numerical Model and Experimental Validation of Vibration-Based De-Icing of a Flat Plate Structure
 
 
Article

Article Versions Notes

Action Date Notes Link
article xml file uploaded 22 May 2020 10:37 CEST Original file -
article xml uploaded. 22 May 2020 10:37 CEST Update https://www.mdpi.com/2226-4310/7/5/62/xml
article pdf uploaded. 22 May 2020 10:37 CEST Version of Record https://www.mdpi.com/2226-4310/7/5/62/pdf
article html file updated 22 May 2020 10:39 CEST Original file -
article html file updated 5 June 2020 03:55 CEST Update -
article html file updated 21 July 2022 05:40 CEST Update https://www.mdpi.com/2226-4310/7/5/62/html
Back to TopTop