What exact formulas are needed to calculate sea level angle of climb from the following information? put formulas used and exact answers. for example, i know the rate of climb is (rate of climb: 6,000 ft/min (30 m/ what is the formula used to get this? this is a physics/aerodynamics question for homework needed in a timely, legible manner (use mathtype if possible. a standard sea level day is listed below:
density (rho): 1.225 kg/m³ (0.00237 slug/ft³), viscosity (μ): 17.3 µpa·s (3.62 × 10⁻⁷ lb s/ft²)
pressure (p): 1013.25 hpa (14.7 lb/ in²), or 29.92" hg, temperature (t): 15 °c (59 °f).
maximum speed: 381 knots (439 mph, 706 km/h) at sea level, clean
cruise speed: 300 knots (340 mph, 560 km/h)
stall speed: 120 knots (138 mph, 220 km/h)
wing area: 506 ft² (47.0 m²) / airfoil: naca 6716
empty weight: 24,959 lb (11,321 kg)
max. takeoff weight: 50,000 lb (22,700 kg)
internal fuel capacity: 11,000 lb (4,990 kg)
powerplant: 2 × turbofans engines producing 9,065 lbs. of thrust each.