To calculate static and dynamic pressure for a wind tunnel lab report, one must understand the Bernoulli equation, which relates these pressures to fluid velocity. Static pressure can be measured directly using a manometer, while dynamic pressure is calculated using the formula q = 0.5 * ρ * V², where ρ is the fluid density and V is the flow velocity. Drag force and lift force can be determined using the coefficients of drag and lift, which depend on the shape of the object and the flow conditions. It's essential to present initial calculations or attempts to facilitate further assistance. Accurate calculations are crucial for analyzing aerodynamic performance in wind tunnel experiments.