Within the Project “K4A Helicopter KA-2HT”, NOVOTECH has provided the Design and Simulation Drop Testing on Landing Gear Skid, in particular developing the Static Analysis with MSC NASTRAN/PATRAN and the Dynamic one with MSC Adams. In particular, NOVOTECH has also simulated the Drop Test of the KA-2HT by means of Multi-Body Dynamic Analysis with MSC ADAMS code, in accordance with regulations CS-27.
Partners:
Capabilities:
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)
MAIN AEROSPACE STRUCTURAL COMPONENT
Preliminary Sizing
Structural Stress Analysis
Structural Fatigue Analysis
Structural Components Design
Finite Element Analysis
Static and Dynamic Experimental Tests
