Author Details

Chajec, Wojciech Celestyn, Instytut Lotnictwa, Poland

  • Vol 3, No 1 (2013) - Experimental techniques in Aeroelasticity and Structural Dynamics
    AEROELASTIC CALCULATION OF INNOVATIVE NON-CONVENTIONAL AIRCRAFT WITH SWINGING CANARD SURFACE
    Abstract  PDF


ISSN 1974-5117