Modal tests
WE OFFER:
- Modal tests of entire structures, aero-elastic scaled models and aircraft structures (e.g. whole aircraft and their components, power plants, propellers, control systems, hydraulic actuators, skin fields and other structures)
- Definition of modal parameters (frequency, mode shape, damping, generalized mass and stiffness)
- Excitation of isolated vibration modes by accommodated sinus excitation
- Sweep harmonic excitation, pulse excitation, white noise excitation
- Graphic display of deformations and nodal lines
- Animation of mode shapes
- Modal parameters corrections for the extra mass and stiffness of the tester
- Orthogonality verification and calculation of vibration mode correlation criteria
- Transfer function definition
- Input data preparation for flutter calculation
EQUIPMENT:
- Mobile facility for modal tests, GVT (Ground Vibration Tests) using PRODERA tester with circuits to excite constructions by eight channel system; response measurement at 256 points
- Software: P-WIN-MODAL to control modal tests
- Software: MOPAR to treat modal test results
STANDARD SPECIFICATIONS:
- Airworthiness and reliability regulations as applied to aircraft specific categories
APPROVAL CERTIFICATES:
- ISO 9001:2000
- Civil Aviation Authority of the Czech Republic (ÚCL) certificate to conduct strength test aircraft airframes and mechanical aircraft articles
CUSTOMERS:
- Companies involved in design and development of aircraft and land transport vehicles
- Engineering companies requiring to verify dynamic properties of their products or parts (experimentally or theoretically)
- Universities and research establishments