GENERAL THEORY OF ESTIMATION OF EXHAUST EMISSIONS WITH IC ENGINE APPLICATIONS
PREDICTION OF ACOUSTIC STRESSES IN AIRCRAFT PANELS - APPLICATION OF ENERGY MODELS
RESULTS OF THE INVESTIGATION OF THE PISTON ENGINES WITH THE CATALYTIC PRECHAMBER
INFLUENCE OF SIMULATED BLADE DAMAGES ON THE HELICOPTER ROTOR LOADES LEVE
WIND TUNNEL AERODYNAMIC TEST OF THE LIGHT AIRCRAFT MODEL AT HIGH ANGLE OF ATTACK
PRACTICAL METHODS OF DYNAMIC OBJECTS IDENTIFICATION PART I. SMALL PERTURBATIONS METHOD
FLIGHTLAB SOFTWARE TOOL FOR MODELLING OF CONTROLLED AIRCRAFT - FIRST EXPERIENCES
THE APPLICATION OF HELICOPTER FORCES ON THE COMBAT ACTIONS OF THE ARMY
CONSIDERATIONS ON STAGES OF AVIATION TURBINE ENGINE TEST PROGRAM
CHANGES OF MI-2 HELICOPTER LEADING TO ACHIEVE SECOND PERFORMANCE CLASS
CURRENT AND FUTURE POSSIBILITIES OF HELICOPTER PILOTS TRAINING IN THE AIR FORCE COLLEGE