NOVOTECH completed a GVT survey on the Vulcanair A – Viator AP600 Aircraft in order to identify its structural dynamic characteristics, and to demonstrate the aircraft’s conformity with the EASA CS-23 norms par. 23.629 “Flutter”. The modal parameters (natural frequencies, damping and mode-shapes) were determined for both stick-free and stick-fixed conditions. NOVOTECH proceeded to test the aircraft structure in two configurations: the Max Zero Fuel Weight (MZFW) and the Max Take-off Weight (MTOW) at Max Fuel and with the installation of two sub-wing pods at the maximum weight condition.
Partners:
Capabilities:
ACOUSTIC AND VIBRATIONS
Experimental Modal Analysis
Real Life Monitoring
Active and Passive Vibration (Design and Testing)
Production of Noise and Vibrations Control System
Statistical Energy Analysis (SEA)
Noise Certification (FAR 36 and ICAO Annex 16)
Material Testing
AEROELASTICITY
GVT-Ground Vibration Testing
Aerolastic Certification with FAA, EASA
Gust Load Calculations
DESIGN, TESTING and CERTIFICATION of GENERAL AVIATION AICRAFT
Preliminary Design and Sizing
Wind Tunnel Testing
Detailed Design and Structural Calculation by Classical Methods and FEM Analysis
Static Testing of Main Components
Certification with FAA and EASA rules
(LSA, VLA, FAR 23 -CS 23, Far 25-CS 25)
