The need to quickly provide assistance to victims of accidents or seriously ill has created the need for the construction of helipads at selected hospitals. Their operation and the conditions of use are governed by regulation of the Ministry of Health on Hospital Emergency Ward (SOR) and rules required by the Civil Aviation Authority.
The direct vicinity of the helipads causes impact of landing and departing helicopters on buildings, people and hospital equipment as well as the construction of the airfield. This article presents vibroacoustic impact of helicopters on helipads’ measurement methods and the results of the preliminary measurements to estimate the impact of Helicopter Air Rescue (LPR) on adjacent buildings and surroundings.
engine in flight basing on signals recorded during groundtests, Journal of KONES, Vol.19, nr 3 (2012).  Golak K.: Validity Check of the Assessment of a Jet Turbine Engine Regulation in Flight Using a Computer Simulation, Solid State Phenomena, Durnten-Zurich 2013.  Lindstedt P., Praktyczna regulacja maszyn i jej teoretyczne podstawy, Wydawnictwo Instytutu Technicznego Wojsk Lotniczych, Warszawa 2010.  Osiowski J., Zarys rachunku operatorowego, teoria i zastosowanie w elektrotechnice, Wydawnictwo Naukowo-Techniczne, Warszawa 1981.  Szczeciński S.: „Napęd
Comparison of Computer-Simulation Results for a Jet Engine with Half-Ideal Gas and Ideal Gas as a Working Medium
Two simulative models for the same jet engine, plus simulation results of deceleration, acceleration and steady states of engine operation during ground tests, are presented in the article. The models differ from each other just with the working medium flowing through the engine. In the first model it was assumed that, while the working medium is flowing through the compressor, the isentropic exponent and average specific heat are functions of average total temperature, whereas, while it is flowing through the combustion chamber, turbine, and nozzle, these are functions of corresponding average temperatures of total pressure and combustion air factor. In the second model the working medium is treated as an ideal gas, with constant values of isentropic exponent and specific heat in some parts of the flow being analyzed.
-destructive thermography-based method to assess gas-turbine blade condition. The Problems of Studying, Testing and Operating Aeronautical Systems. Vol. 8, Chapter 8. AFIT, Warszawa 2012 (in Polish).  Lindstedt P., Golak K., Borowczyk H.: A complex method to predict in-flight functional properties of an aircraft turbine engine on the basis of groundtests. The Problems of Studying, Testing and Operating Aeronautical Systems. Vol. 8, Chapter 11, AFIT, Warszawa 2012 (in Polish).  Lindstedt P., Grądzki R., Borowczyk H.: A parametric method to diagnose a turbo-machine’s blade, with non
Design and Experiment for Electric Load Simulator, 2010 3rd International Conference on Advanced Computer Theory and Engineering (lCACTE).  XIN, W.—ZHU, F. D. : Load Simulator Design and GroundTest of Near Space Hypersonic Vehicle, Journal of System Simulation 21 No. 19 (Oct 2009).  YONG, H.—LU, X.—JIE, Y.—LI, S. : The Controller Designed for Motor Servo Loading System based on ITAE, 1994-2010 China academic Journal.  PENG, L.—HUI, L. : Controller Design for Missile Rudder Electric Loading Simulation System, Journal of Computer, Measurement and Control
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Transportation Systems (ITSC) , Maui, HI, USA, 4-7 Nov. 2018, DOI: 10.1109/ITSC.2018.8569938 10. Marilisa, B., Luigi, P., Nicola, B. G. (2018) C-ITS communication: an insight on the current research activities in the European Union. International Journal of Transportation Systems , 3(1), 52-63. ISSN: 2534-8876 11. Németh, H., Háry, A., Szalay, Zs., Tihanyi, V., Tóth, B. (2018) Proving groundtest scenarios in mixed virtual and real environment for highly automated driving , Research paper for Automotive Proving Ground Zala Ltd. 12. PEGASUS (2018) Project description, https
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