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...
EP ID EP71137
DOI 10.5604/12314005.1137901
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How To Cite
Mariusz Cygnar (2012). ANALYSIS OF PARAMETERS OF THE ENGINE WORKING
IN TWO THERMODYNAMIC CYCLES. Journal of KONES, 19(2),
95-102. https://europub.co.uk./articles/-A-71137
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TRAFFIC DISTRIBUTION INTO TRANSPORT NETWORK FOR DEFINED SCENARIOS OF TRANSPORT SYSTEM DEVELOPMENT IN ASPECT OF ENVIRONMENTAL PROTECTION
IMPACT OF AN EXTERNAL, SO CALLED BOX, MODULE ON GASES COMPOSITION OF THE ROVER 2.0 CDTI ENGINE
INVESTIGATION OF AVIONIC EVENTS WITH USE OF INFORMATION FROM ON-BOARD RECORDERS OF FLIGHT PARAMETERS
THE NUMERICAL SIMULATION OF THE PYROTECHNIC ACTUATOR FOR THE ACTIVE BUMPER
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...