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Contents of the Thermodynamics and Governing Equations PDF

List of 19 Thermodynamics and Governing Equations Formulas

Choked Mass Flow Rate

Choked Mass Flow Rate given specific heat ratio

Efficiency of cycle

Efficiency of Joule cycle

Enthalpy of Ideal Gas at given Temperature

Heat Capacity Ratio

Internal Energy of Perfect Gas at given Temperature

Mach Angle

Mach Number

Max work output in Brayton cycle

Pressure Ratio

Specific Heat of mixed out gas

Speed of Sound

Stagnation enthalpy

Stagnation Temperature

Stagnation Velocity of Sound

Stagnation Velocity of Sound given Specific Heat at Constant Pressure

Stagnation Velocity of Sound given Stagnation Enthalpy

Work ratio in practical cycle

Variables used in Thermodynamics and Governing Equations PDF

a Speed of Sound (Meter per Second)
a_o Stagnation Velocity of Sound (Meter per Second)
A_throat Nozzle Throat Area (Square Meter)
C_p Specific Heat Capacity at Constant Pressure (Joule per Kilogram per K)
C_p Specific Heat Capacity at Constant Pressure (Joule per Kilogram per K)
C_p,m Specific Heat of Mixed Gas (Joule per Kilogram per K)
C_p,β Specific Heat of Bypass Air (Joule per Kilogram per K)
C_pe Specific Heat of Core Gas (Joule per Kilogram per K)
C_v Specific Heat Capacity at Constant Volume (Joule per Kilogram per K)
h Enthalpy (Kilojoule per Kilogram)
h₀ Stagnation Enthalpy (Kilojoule per Kilogram)
m Mass Flow Rate (Kilogram per Second)
M Mach Number
ṁ_choke Choked Mass Flow Rate
P_f Final Pressure (Pascal)
P_i Initial Pressure (Pascal)
P_o Throat Pressure (Pascal)
P_R Pressure Ratio
Q Heat (Kilojoule)
T Temperature (Kelvin)
T₀ Stagnation Temperature (Kelvin)
T₀ Stagnation Temperature (Kelvin)
T_B1 Temperature at Inlet of Compressor in Brayton (Kelvin)
T_B3 Temperature at Inlet to Turbine in Brayton Cycle (Kelvin)
T_s Static Temperature (Kelvin)
U Internal Energy (Kilojoule per Kilogram)
u₂ Flow Velocity Downstream of Sound (Meter per Second)
U_fluid Velocity of Fluid Flow (Meter per Second)
V_b Speed of Object (Meter per Second)
W Work Ratio
W_c Compressor Work (Kilojoule)
W_Net Net Work Output (Kilojoule)
W_pmax Maximum Work done in Brayton Cycle (Kilojoule)
W_T Turbine Work (Kilojoule)
β Bypass Ratio
γ Heat Capacity Ratio
γ Specific Heat Ratio
η_c Compressor Efficiency
η_cycle Efficiency of Cycle
η_{joule cycle} Efficiency of Joule Cycle
η_turbine Turbine Efficiency
μ Mach Angle (Degree)

Constants, Functions and Measurements used in Thermodynamics and Governing Equations PDF

Constant: [R-Dry-Air], 287.058
Specific Gas Constant for Dry Air
Constant: [R], 8.31446261815324
Universal gas constant
Function: asin, asin(Number)
The inverse sine function, is a trigonometric function that takes a ratio of two sides of a right triangle and outputs the angle opposite the side with the given ratio.
Function: sin, sin(Angle)
Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse.
Function: sqrt, sqrt(Number)
A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.
Measurement: Temperature in Kelvin (K)
Temperature Unit Conversion
Measurement: Area in Square Meter (m²)
Area Unit Conversion
Measurement: Pressure in Pascal (Pa)
Pressure Unit Conversion
Measurement: Speed in Meter per Second (m/s)
Speed Unit Conversion
Measurement: Energy in Kilojoule (KJ)
Energy Unit Conversion
Measurement: Angle in Degree (°)
Angle Unit Conversion
Measurement: Specific Heat Capacity in Joule per Kilogram per K (J/(kg*K))
Specific Heat Capacity Unit Conversion
Measurement: Mass Flow Rate in Kilogram per Second (kg/s)
Mass Flow Rate Unit Conversion
Measurement: Specific Energy in Kilojoule per Kilogram (kJ/kg)
Specific Energy Unit Conversion

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