Which of the following is the correct formula for lift of an aircraft?

• A. L=\(\frac{1}{2}\)ρV2SCl
• B. L=\(\frac{1}{2}\)V2SCl
• C. L=\(\frac{1}{2}\)ρV2Cl
• D. L=\(\frac{1}{2}\)PV2SCl