I need help with this.​

What is the stall speed at sea level of an airplane that weights 10000 lbs., has a wing area of 300ft^2, and a maximum lift coefficient of 1.4? what is the stall speed if flaps that double cl,max are applied?

What are two different ways you could find the value of a? explain these methods.

Which of the following bonds would be most polar? a. c-i b. c-br c. c-cl d. c-f e. c-o