Marcin Noga, Bronisław Sendyka
Airplane wing load control systems are designed for modification/redistribution of aerodynamic loads in order to decrease risk of structural damage in conditions of excessive loads, to improve passenger comfort in turbul...
Marcin Noga, Bronisław Sendyka (2013). NEW DESIGN OF THE FIVE-STROKE SI ENGINE. Journal of KONES, 20(1), 239-246. https://europub.co.uk/articles/-A-65259
For faster login or register use your social account.
DESIGN OF THE RAPID COMPRESSION MACHINES FOR COMBUSTION RESEARCHES IN SPARK IGNITION ENGINES
THE ESTIMATION OF THE INCREASED LIMITATION OF THE VISIBILITY IN THE LIGHT COMMERCIAL VEHICLES
MEASUREMENTS OF PRESSURE IN FRONT OF SHOCK WAVE – ASSESSMENT OF METHODOLOGY INFLUENCE ON THE MEASUREMENT RESULTS ON THE BASIS OF EXPERIMENTS WITH THE SHOCK TUBE
ENERGY SCAVENGING IN A VEHICLE’S EXHAUST SYSTEM
MODIFICATION OF AERODYNAMIC WING LOADS BY FLUIDIC DEVICES
Airplane wing load control systems are designed for modification/redistribution of aerodynamic loads in order to decrease risk of structural damage in conditions of excessive loads, to improve passenger comfort in turbul...