Cavitation is a critical phenomenon in hydrodynamic applications, significantly influencing the performance and durability of hydrofoils. This study presents a numerical investigation of cavitation over hydrofoils, focusing on the effects of thickness and camber, using the interPhaseChangeFoam solver within the OpenFOAM framework. The numerical setup was validated against experimental data for the NACA66(mod) hydrofoil. Simulations were performed at a fixed angle of attack of 4° under two cavitation numbers, σ = 0.84 and σ = 0.91 using the Schnerr–Sauer cavitation model with a vapor pressure of 2420 Pa. To assess thickness effects, symmetric hydrofoils NACA0012, NACA0016, and NACA0020 were analyzed, while camber effects were examined using hydrofoils of identical thickness but varying camber, NACA0012, NACA2412, and NACA4412. Results show that cambered and thicker hydrofoils develop more extensive cavitation regions. Increasing the cavitation number generally leads to higher lift coefficients, with the effect more pronounced for cambered profiles. Greater camber promotes earlier cavitation inception, a larger cavity extent, and higher lift, with NACA4412 achieving the highest lift coefficients of approximately CL = 0.74 and 0.79 at σ = 0.84 and 0.91, respectively. Increased thickness also enlarges the cavitation region but generally results in lower lift, as observed for NACA0020, which exhibited lift coefficients of approximately CL = 0.31 and 0.34 at σ = 0.84 and 0.91, respectively. Increasing the cavitation number from σ = 0.84 to 0.91 reduced drag for all profiles by up to about 23% while preserving lift in cambered foils.
Ethics committee approval was not required for this study because there was no study on animals or humans.
Cavitation is a critical phenomenon in hydrodynamic applications, significantly influencing the performance and durability of hydrofoils. This study presents a numerical investigation of cavitation over hydrofoils, focusing on the effects of thickness and camber, using the interPhaseChangeFoam solver within the OpenFOAM framework. The numerical setup was validated against experimental data for the NACA66(mod) hydrofoil. Simulations were performed at a fixed angle of attack of 4° under two cavitation numbers, σ = 0.84 and σ = 0.91 using the Schnerr–Sauer cavitation model with a vapor pressure of 2420 Pa. To assess thickness effects, symmetric hydrofoils NACA0012, NACA0016, and NACA0020 were analyzed, while camber effects were examined using hydrofoils of identical thickness but varying camber, NACA0012, NACA2412, and NACA4412. Results show that cambered and thicker hydrofoils develop more extensive cavitation regions. Increasing the cavitation number generally leads to higher lift coefficients, with the effect more pronounced for cambered profiles. Greater camber promotes earlier cavitation inception, a larger cavity extent, and higher lift, with NACA4412 achieving the highest lift coefficients of approximately CL = 0.74 and 0.79 at σ = 0.84 and 0.91, respectively. Increased thickness also enlarges the cavitation region but generally results in lower lift, as observed for NACA0020, which exhibited lift coefficients of approximately CL = 0.31 and 0.34 at σ = 0.84 and 0.91, respectively. Increasing the cavitation number from σ = 0.84 to 0.91 reduced drag for all profiles by up to about 23% while preserving lift in cambered foils.
Ethics committee approval was not required for this study because there was no study on animals or humans.
Birincil Dil | İngilizce |
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Konular | Akışkan Akışı, Isı ve Kütle Transferinde Hesaplamalı Yöntemler (Hesaplamalı Akışkanlar Dinamiği Dahil), Çoklu Fizik Akışları (Çok Fazlı ve Reaksiyona Giren Akışlar Dahil), Türbülanslı Akışlar, Akışkan Mekaniği ve Termal Mühendislik (Diğer), Sayısal Modelleme ve Mekanik Karakterizasyon |
Bölüm | Research Articles |
Yazarlar | |
Erken Görünüm Tarihi | 11 Eylül 2025 |
Yayımlanma Tarihi | 15 Eylül 2025 |
Gönderilme Tarihi | 5 Ağustos 2025 |
Kabul Tarihi | 9 Eylül 2025 |
Yayımlandığı Sayı | Yıl 2025 Cilt: 8 Sayı: 5 |