AE 370 Equations and Values
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Last updated 1:04 AM on 9/18/26
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35 Terms
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Ideal Gas Law
2
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Dynamic Pressure
3
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Coefficient of Lift
4
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Coefficient of Drag
5
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Coefficient of Moment
6
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Reynolds’ Number
7
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Mach Number
8
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Speed of Sound for an Ideal Gas
9
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Coefficient of Lift (using angle of attack)
10
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Planform Area
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Aspect Ratio
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Taper Ratio
13
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Coefficient of Induced Drag
14
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Parasite Drag
15
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Drag Polar
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General Thrust
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Power Avaliable
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General Specific Fuel Consumption
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Power - Propeller Driven
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Pressure to Density Ratio - Propeller Driven + Turbojet
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Propulsive Power - Propeller Driven
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Thrust - Turbojet
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Mass Flow Rate - Turbojet
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Thrust-Specific Fuel Consumption - Turbojet
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Std Sea Level Pressure - English
2116 lb/ft^2
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Std Sea Level Pressure - Metric
101.3 KPa
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Std Sea Level Temperature - English
59 F
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Std Sea Level Temperature - Metric
15 C
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Std Sea Level Density - English
0.002377 slug/ft^3
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Std Sea Level Density - Metric
1.225 kg/m^3
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Ideal Gas Constant (air) - English
1716 ft lb/slugs R
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Ideal Gas Constant (air) - Metric
287 J/kg K
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Ratio of Specific Heats
1.4
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hp ----> ft lb/s
1 hp = 550 ft lb/s
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mile ----> feet
1 mile = 5280 ft