Download Normal Shock Wave PDF | Free Normal Shock Wave PDF

Related PDFs (11)

Elementary Flows

Formulas : 16 Size : 335 kb

Elliptical Lift Distribution

Formulas : 20 Size : 349 kb

Flow and Lift Distribution

Formulas : 24 Size : 394 kb

Flow over Airfoils and Wings

Formulas : 26 Size : 421 kb

Fundamentals of Inviscid and Incompressible Flow

Formulas : 16 Size : 342 kb

Governing Equations and Sound Wave

Formulas : 18 Size : 378 kb

Lift Distribution

Formulas : 30 Size : 426 kb

Lifting Flow over Cylinder

Formulas : 10 Size : 300 kb

Nonlifting Flow over Cylinder

Formulas : 10 Size : 296 kb

Oblique Shock and Expansion Waves

Formulas : 20 Size : 390 kb

Three-Dimensional Incompressible Flow

Formulas : 29 Size : 419 kb

Contents of the Normal Shock Wave PDF

List of 35 Normal Shock Wave Formulas

Characteristic Mach Number

Characteristic Mach Number behind Shock

Critical Speed of Sound from Prandtl Relation

Density ahead of Normal Shock using Normal Shock Momentum Equation

Density behind Normal Shock given Upstream Density and Mach Number

Density behind Normal Shock using Normal Shock Momentum Equation

Density Downstream of Shock Wave using Continuity Equation

Density Ratio across Normal Shock

Density Upstream of Shock Wave using Continuity Equation

Downstream Velocity using Prandtl Relation

Enthalpy ahead of Normal Shock from Normal Shock Energy Equation

Enthalpy behind Normal Shock from Normal Shock Energy Equation

Enthalpy Difference using Hugoniot Equation

Entropy Change across Normal Shock

Flow Velocity Downstream of Shock Wave using Continuity Equation

Flow Velocity Upstream of Shock Wave using Continuity Equation

Mach Number behind Shock

Mach Number given Impact and Static Pressure

Pressure Ratio across Normal Shock

Relation between Mach Number and Characteristic Mach Number

Shock Strength

Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula

Static Enthalpy behind Normal Shock for given Upstream Enthalpy and Mach Number

Static Enthalpy Ratio across Normal Shock

Static Pressure ahead of Normal Shock using Normal Shock Momentum Equation

Static Pressure behind Normal Shock for given Upstream Pressure and Mach Number

Static Pressure behind Normal Shock using Normal Shock Momentum Equation

Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number

Temperature Ratio across Normal Shock

Upstream Velocity using Prandtl Relation

Velocity ahead of Normal Shock by Normal Shock Momentum Equation

Velocity ahead of Normal Shock from Normal Shock Energy Equation

Velocity behind Normal Shock

Velocity behind Normal Shock by Normal Shock Momentum Equation

Velocity behind Normal Shock from Normal Shock Energy Equation

Variables used in Normal Shock Wave PDF

a_cr Critical Speed of Sound (Meter per Second)
h₁ Enthalpy Ahead of Normal Shock (Joule per Kilogram)
h₂ Enthalpy Behind Normal Shock (Joule per Kilogram)
H_r Static Enthalpy Ratio Across Normal Shock
M Mach Number
M₁ Mach Number Ahead of Normal Shock
M₂ Mach Number Behind Normal Shock
M_cr Characteristic Mach Number
M1_cr Characteristic Mach Number Ahead of Shock
M2_cr Characteristic Mach Number Behind Shock
p₀₁ Stagnation Pressure Ahead of Normal Shock (Pascal)
p₀₂ Stagnation Pressure Behind Normal Shock (Pascal)
P₁ Static Pressure Ahead of Normal Shock (Pascal)
P₂ Static pressure Behind Normal shock (Pascal)
P_r Pressure Ratio Across Normal Shock
p_st Static Pressure (Pascal)
q_c Impact Pressure (Pascal)
R Specific Gas Constant (Joule per Kilogram per K)
T₁ Temperature Ahead of Normal Shock (Kelvin)
T₂ Temperature Behind Normal Shock (Kelvin)
T_r Temperature Ratio Across Normal Shock
u_f Fluid Velocity (Meter per Second)
V₁ Velocity Upstream of Shock (Meter per Second)
V₂ Velocity Downstream of Shock (Meter per Second)
γ Specific Heat Ratio
ΔH Enthalpy Change (Joule per Kilogram)
Δp_str Shock Strength
ΔS Entropy Change (Joule per Kilogram K)
ρ₁ Density Ahead of Normal Shock (Kilogram per Cubic Meter)
ρ₂ Density Behind Normal Shock (Kilogram per Cubic Meter)
ρ_r Density Ratio Across Normal Shock

Constants, Functions and Measurements used in Normal Shock Wave PDF

Function: ln, ln(Number)
The natural logarithm, also known as the logarithm to the base e, is the inverse function of the natural exponential function.
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: Pressure in Pascal (Pa)
Pressure Unit Conversion
Measurement: Speed in Meter per Second (m/s)
Speed Unit Conversion
Measurement: Heat of Combustion (per Mass) in Joule per Kilogram (J/kg)
Heat of Combustion (per Mass) Unit Conversion
Measurement: Specific Heat Capacity in Joule per Kilogram per K (J/(kg*K))
Specific Heat Capacity Unit Conversion
Measurement: Density in Kilogram per Cubic Meter (kg/m³)
Density Unit Conversion
Measurement: Specific Entropy in Joule per Kilogram K (J/kg*K)
Specific Entropy Unit Conversion
Measurement: Specific Energy in Joule per Kilogram (J/kg)
Specific Energy Unit Conversion

Download Now!