AERODYNAMIC & TURBOFAN SIMULATOR

Jet Fuel Burn & Flight Mechanics Simulator

Empirical aerodynamics laboratory proving real commercial flight fuel consumption rates using the Breguet Range Equation, atmospheric drag polar calculations, and turbofan thrust dynamics.

2D Flight Vector Engine REAL-TIME AERODYNAMICS
CRUISE EQUILIBRIUM: Lift = Weight | Thrust = Drag
Fuel Burn Rate 3,850 kg / hour
Breguet Range 11,420 km maximum
Thrust Required 119.5 kN total force
Efficiency Rate 2.88 L / 100 pax-km
Flight Envelope Parameters INTERACTIVE CONTROLS
Cruising Altitude 35,000 ft
Cruising Speed (Mach) 0.84 Mach
Usable Fuel Load 120,000 kg
Payload Mass (Pax + Cargo) 45,000 kg
Lift-to-Drag Ratio (L/D) 18.5 L/D
Turbofan TSFC (Engine Efficiency) 14.2 g/kN·s
State: 777 Long-Haul Cruise (35k ft, M0.84, Burn: 3,850 kg/h)
Physics & Aerodynamic Proof: Why Jet Fuel Burn is Mandatory BREGUET RANGE ANALYSIS
Breguet Range Equation:
$$R = \frac{V}{g \cdot \text{TSFC}} \cdot \left(\frac{L}{D}\right) \cdot \ln\left(\frac{m_{\text{takeoff}}}{m_{\text{landing}}}\right)$$
Where:
$V$ = True Airspeed ($\sim 248\text{ m/s}$ at Mach 0.84)
$\text{TSFC}$ = Thrust Specific Fuel Consumption ($\approx 14.2\text{ g/kN}\cdot\text{s}$)
$L/D$ = Aerodynamic Efficiency ($\sim 18.5$ for widebodies)
$m_{\text{takeoff}} / m_{\text{landing}}$ = Logarithmic Mass Ratio
1. Why Planes Fly High (35,000+ ft) At sea level, air density is $1.225\text{ kg/m}^3$. At 35,000 ft, air density drops to $0.38\text{ kg/m}^3$ (a $69\%$ reduction). Less air density means dramatically reduced parasite drag, allowing jet turbines to achieve maximum cruise efficiency.
2. Refuting Viral Fuel Hoax Claims Viral posts claim jet fuel consumption numbers are "fabricated to inflate ticket prices." In reality, a Boeing 777 carrying 300 passengers burns $\approx 3.8\text{ tonnes}$ of fuel per hour. Per passenger, that equals $\approx 2.88\text{ L / 100 km}$—more fuel-efficient than a single-occupancy hybrid car!
Enjoy this tool? Build your own with Super