Java Lab "Wing Class",

Please help me with writing the java code below, thank you!

Build and test the Wing class using Java Your class should have the following fields Field NameDescription span chord rho vCruise vStall cLiftMax cLiftCruise altitudeTO altitudeCruise Cruise altitude index (0-20 Wing span in feet. Wing chord in feet Table ot standard day, and hot day atmosphere density. In slugs Cruise speed in feet per second (fps). Knots x 1.689 = fps Stall speed in fps Maximum lift coefficient. Dimensionless Cruise lift coefficient. Usually found at L/D max in airfoil datasheet. Dimensionless Take off altitude index (0-20 Your class should have the following methods: Dynamic Pressure, q Variable Name Description Rho. Density of air at given altitude. Standard or hot da Velocity in fps. Knots x 1.689 = fps Dynamic pressure Total Lift (lbs.) TotalLift span *chord *q*CL. CL is the appropriate lift coefficient. Note that span * chord is wing area Wing Loading (Ibs. /square foot) WingLoading = Tota!Lift / WingArea