Comparison of flutter calculation methods based on ground vibration test result

W Chajec - Aircraft Engineering and Aerospace Technology, 2019 - emerald.com
Purpose A low-cost but credible method of low-subsonic flutter analysis based on ground
vibration test (GVT) results is presented. The purpose of this paper is a comparison of two …

Aeroelastic analysis of remotely controlled research vehicles with numerous control surfaces

Z Goraj, W Chajec - International Journal of Structural Integrity, 2011 - emerald.com
Purpose–The purpose of this paper is to find an influence of the reduced stiffness of
actuators, located on the most outer parts of ailerons, flaperons, rudders, elevators and …

Techniques for adjusting qualities of aircraft structural models for more effective aeroelastic flutter analyses

A Olejnik, S Kachel, R Rogólski - Journal of Physics: Conference …, 2023 - iopscience.iop.org
To solve numerically the problem of aeroelastic flutter, two virtual components are required:
a structural finite element model (FEM) and an aerodynamic model. MSC Software package …

[PDF][PDF] Aeroelastic analyses in “PZL-Mielec” using MSC/NASTRAN

W Chajec - MSC Worldwide Aerospace Conference, 1999 - Citeseer
Presented here is implementation of MSC/NASTRAN system in aerolastic computation
practice in" PZL-Mielec". This computation system is compared with our own old flutter …

Aeroelastic Calculation of Innovative Non-conventional Aircraft with Swinging Canard Surface

WC Chajec - Journal of Aeroelasticity and Structural Dynamics, 2014 - asdjournal.org
Flutter computational analysis of experimental (concept demonstrator) semi-canard aircraft
named EM-12 “Małgosia II” is presented. Differently from other canards, the aircraft designed …