QUALITATIVE BEHAVIOR OF EIGENFREQUENCIES FOR FREE VIBRATION OF AEROSPACE VEHICLE APPENDAGES

INVESTIGATION OF HELICOPTER STABILITY CONSIDERING THE EFFECT OF ITS HYDRAULIC SERVOACTUATOR AND AUTOPILOT

INVESTIGATION OF LATERAL FLYING QUALITIES OF AIRCRAFT

AN APPROACH TO THE OPTIMUM DESIGN OF THE ROTOR SYSTEM OF SINGLE-ROTOR HELICOPTERS

COMPUTER AIDED ANALYSIS OF COMPLEX VIBRATION SIGNATURE OF TURBOJET ENGINES

MODELLING OF VIBRATION DAMPING IN COMPOSITE STRUCTURES

SOME ASPECTS OF AN EXPERIMENTAL INVESTIGATION ON COMPOSITE AEROBATIC AIRCRAFT STRUCTURE.

VIBRATION ANALYSIS OF A FLAT PLATE UNDER AERODYNAMIC LOADING

ANALYSIS OF WING-FUSELAGE STRUCTURE INTERACTION UNDER ASYMMETRIC TORQUE

Speculation of local aerodynamic loads on helicopter rotor blade in forward flight