Dr Bond Airplane

1) Standard Sea Level Pressure

2116 lb/ft² | 101325Pa

1) Standard Sea Level Temperature

518.67 R | 288.15 K

1) Standard Sea Level Density

.002377 slug/ft³ | 1.225 kg/m³

1) Idea Gas Constant

1716 ft*lb/slug*R | 287 J/kg*K

1) Ratio of Specific Heats

1.4 | 1.4

2) Drag Polar

2) Zero Lift Drag

2) Wing Taper Ratio

2) Reynolds Number

2) Ideal Gas Law

2) Induced Drag

2) Aspect Ratio

2) Drag Coefficient

2) Planform Area

2) Lift Coefficient

2) Dynamic Air Pressure

2) 2D Lift Coefficient

2) Mach Number

2) Free Stream Speed of Sound

3) Standard Trust Equation

3) Engine Power

3) Specific fuel consumption for reciprocating engines

3) Actual Engine Power

3) Power Ratio

3) Power Available

3) Turbojet thrust

3) Mass Flow Rate

3) Thrust Ratio

3) Thrust Specific Fuel Consumption for jets

3) Bypass Ratio

3) Turboprop Power Available

4) Load Factor

5) Drag

5) Weight

5) Zero Lift drag coefficient for L/D max

5) Thrust Required

5) Rate of climb for Vv

Excess Power

5) Rate of climb for excess power

5) Tangent theta

5) Stall Speed

5) C_Lmax flaps

5) Delta C_LMax