- Tytuł:
- An assessment of the transient effect on helicopter main rotor stability and power demand
- Autorzy:
-
Raczyński, Radosław
Siadkowska, Ksenia
Ścisłowski, Karol
Wendeker, Mirosław - Powiązania:
- https://bibliotekanauki.pl/articles/2202519.pdf
- Data publikacji:
- 2022
- Wydawca:
- Polskie Towarzystwo Naukowe Silników Spalinowych
- Tematy:
-
propulsion
rotor
power demand
helicopter
transient effect
napęd
wirnik
zapotrzebowanie na moc
śmigłowiec
efekt przejściowy - Opis:
- The researched object is a helicopter main rotor with blades of variable geometric twist characteristics. Variable torsion refers to systems of actuators made of shape memory alloys. The presented numerical analyses allow for evaluating both the dynamics of the rotor in transient states, i.e. in the zone between the static phase and the full activation phase and the impact of the change on the pulsation of the amplitude of the necessary power generated by the rotor corresponding the flight state, and thus covering the demand by the disposable power generated by the engine. This study follows a methodology of numerical analyses based on Multi Body Dynamics and the Finite Element Method and uses fluid mechanics elements and algorithms to analyze lift generation, compiled in a single computational environment referring to the same period of time.
- Źródło:
-
Combustion Engines; 2022, 61, 4; 23--28
2300-9896
2658-1442 - Pojawia się w:
- Combustion Engines
- Dostawca treści:
- Biblioteka Nauki
Artykuł