Hlaziya Ukusebenza Kwe-Airfoil Nge-Vortex Panel Method
Lolu hlelo lokusebenza lusebenzisa indlela yephaneli ye-vortex ukubala ukugeleza kwe-inviscid, okungenakucindezelwa eduze kwe-NACA yezinhlamvu zomoya ezinamadijithi angu-4. Noma ngabe ungumfundi, unjiniyela, noma umthandi wendiza, ikunikeza indlela esheshayo neguquguqukayo yokufunda ukuziphatha kwe-aerodynamic.
✈️ Izici ezibalulekile:
Xazulula ukugeleza kuzungeze i-NACA enamadijithi angu-4 ama-airfoil ochungechunge
Khetha phakathi kwamaphethelo alandelayo avulekile noma avaliwe
Yenza ngokwezifiso i-angle yokuhlasela kanye nenani lamaphaneli (ama-node)
Buka imininingwane yokusabalalisa ingcindezi
Bona ngeso lengqondo ukugeleza nokugeleza kwamaphethini okujikeleza
Bala ama-coefficients angukhiye:
Lift coefficient (CL)
Ama-Moment coefficients (CM)
Ukujikeleza (Γ)
🛠️ Yakhelwe abathanda i-Aerodynamics:
Ilungele izitshudeni zasemkhathini, abasaqalayo be-CFD, nanoma ubani ohlola izindlela zamaphaneli zakudala ngaphandle kwenkimbinkimbi yezixazululi ezigcwele ze-CFD.
Uhlelo lokusebenza lusebenzisa indlela yephaneli ukubala ukugeleza mayelana nama-airfoil ochungechunge lwamadijithi angu-4 we-NACA.
Kubuyekezwe ngo-
Mey 11, 2025