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Michał Kawalec
Michał Kawalec
Instytut Lotnictwa
Verified email at ilot.lukasiewicz.gov.pl
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Cited by
Cited by
Year
Status report on high temperature fuel cells in Poland–Recent advances and achievements
J Molenda, J Kupecki, R Baron, M Blesznowski, G Brus, T Brylewski, ...
International Journal of Hydrogen Energy 42 (7), 4366-4403, 2017
672017
Development of gasturbine with detonation chamber
P Wolański, P Kalina, W Balicki, A Rowiński, W Perkowski, M Kawalec, ...
Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation …, 2018
302018
Applications of the continuously rotating detonation to combustion engines at the Łukasiewicz-Institute of Aviation
M Kawalec, W Perkowski, B Łukasik, A Bilar, P Wolański
Combustion Engines 61, 2022
142022
Development of a liquid-propellant rocket powered by a rotating detonation engine
M Kawalec, P Wolański, W Perkowski, A Bilar
Journal of Propulsion and Power 39 (4), 554-561, 2023
122023
Aircraft emissions during various flight phases
P Głowacki, M Kawalec
Combustion Engines 54, 2015
82015
Experimental research of performance of combined cycle rotating detonation rocket-ramjet engine
P Wolański, M Kawalec
Proc. 27th ICDERS, 2019
72019
Wave direction studies in rotating detonation engine
M Kawalec
Proceedings of the 27th International Colloquium on the Dynamics of …, 2019
72019
Study on kerosene atomization process under a high speed air stream
W Perkowski, A Irzycki, K Snopkiewicz, Ł Grudzień, M Kawalec
Journal of KONES 18, 341-347, 2011
72011
Development of rocket engines with detonation combustion chamber
M Kawalec, W Perkowski, P Wolański
Research on detonative propulsion in Poland, ed. Wolański P, 163-181, 2021
62021
Development of gasturbine with detonation chamber. Detonation control for propulsion, Pulse detonation and rotating detonation engines
P Wolański, P Kalina, W Balicki, A Rowiński, W Perkowski, M Kawalec, ...
Springer, 2018
62018
Assessment of the airframe systems affecting safety risks caused by large aircraft
W Balicki, P Głowacki, M Kawalec
Journal of KONES 23 (1), 39-46, 2016
62016
Research of the rocket engine with detonation chamber
M Kawalec, P Wolański
26th ICDERS, 2017
52017
Estimating emissions of harmful exhaust components by aircraft engines during the takeoff and landing cycle in airport space
P Głowacki, P Kalina, M Kawalec
Transactions on Aerospace Research 2021 (2), 63-70, 2021
42021
Quantitative emissions of NOX, CO and CO2 during aircraft operations
P Glowacki, M Kawalec
30th Congress of the International Council of the Aeronautical Sciences, ICAS, 2016
32016
Możliwości rozwoju silników turbinowych z detonacyjną komorą spalania
P Wolański, P Kalina, W Balicki, A Rowiński, W Perkowski, M Kawalec, ...
Prace Instytutu Lotnictwa, 202--214, 2016
32016
Aircraft fuel consumption and emissions during cruise, effect of the jet stream
P Głowacki, M Kawalec
Journal of KONES 22 (2), 63--70, 2015
32015
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
W Perkowski, A Irzycki, M Kawalec, B Łukasik, K Snopkiewicz
Journal of KONES 20 (4), 333--340, 2013
32013
Development of Rocket Engine with Continuously Rotating Detonation supplied by Liquid Propellants
M Kawalec, P Wolański
Proceeding of EUCASS, Lille, France 27, 0
3
Comparing methods of calculating aircraft engine emissions of harmful exhaust components during the takeoff and landing cycle in the airspace of an airport
P Głowacki, P Kalina, M Kawalec
Transactions on Aerospace Research 2022 (2), 62-68, 2022
22022
The influence of the shape of the combustion chamber on exhaust gases toxicity in T370 engine
P Kalina, M Kawalec
Journal of KONES 22 (2), 104-108, 2015
22015
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