Calculator A to Z

Download Normal Shock Wave PDF

  1. FREE to download!
  2. Examples Included!
  3. With Live Calculator Link!
  4. Supports Unit Conversion!
  5. Mobile friendly PDFs!
Physics PDFsChemistry PDFsEngineering PDFsFinancial PDFsMath PDFs
Aerospace PDFsBasic Physics PDFsMechanical PDFs
Aerodynamics PDFsAircraft Mechanics PDFsOrbital Mechanics PDFsPropulsion PDFs
Compressible Flow PDFsTwo Dimensional Incompressible Flow PDFs
   Normal Shock Wave PDF
Formulas : 35
Size : 471 kb
FREE Download
Share

Related PDFs (47)

Aerodynamic Design
Formulas : 13   Size : 322 kb
Aerodynamic Parameters
Formulas : 11   Size : 298 kb
Aircraft Dynamics Nomenclature
Formulas : 18   Size : 381 kb
Atmosphere and Gas Properties
Formulas : 14   Size : 323 kb
Circular Orbits
Formulas : 18   Size : 348 kb
Climbing Flight
Formulas : 16   Size : 332 kb
Compressor
Formulas : 14   Size : 338 kb
Design Process
Formulas : 19   Size : 401 kb
Efficiency Metrics
Formulas : 12   Size : 325 kb
Elementary Flows
Formulas : 16   Size : 335 kb
Elliptical Lift Distribution
Formulas : 20   Size : 349 kb
Elliptical Orbits
Formulas : 23   Size : 0 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 : 0 kb
Governing Equations and Sound Wave
Formulas : 18   Size : 383 kb
High Load Factor Maneuver
Formulas : 17   Size : 344 kb
Hyperbolic Orbits
Formulas : 11   Size : 0 kb
Jet Airplane
Formulas : 17   Size : 374 kb
Lateral Control
Formulas : 10   Size : 296 kb
Lift and Drag Polar
Formulas : 21   Size : 359 kb
Lift and Drag Requirements
Formulas : 19   Size : 346 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
Parabolic Orbits
Formulas : 14   Size : 0 kb
Preliminary Aerodynamics
Formulas : 17   Size : 374 kb
Preliminary Design
Formulas : 27   Size : 423 kb
Propeller Driven Airplane
Formulas : 22   Size : 384 kb
Pull Up and Pull Down Maneuver
Formulas : 12   Size : 283 kb
Rocket Propulsion
Formulas : 33   Size : 335 kb
Stick Forces and Hinge Moments
Formulas : 23   Size : 369 kb
Structural Design
Formulas : 9   Size : 298 kb
Tail Contribution
Formulas : 19   Size : 334 kb
Take Off and Landing
Formulas : 20   Size : 394 kb
Thermodynamics and Governing Equations
Formulas : 19   Size : 407 kb
Three Dimensional Incompressible Flow
Formulas : 29   Size : 419 kb
Thrust and Power Requirements
Formulas : 19   Size : 347 kb
Thrust Generation
Formulas : 21   Size : 360 kb
Turbofans
Formulas : 10   Size : 270 kb
Turbojets
Formulas : 14   Size : 306 kb
Turning Flight
Formulas : 13   Size : 303 kb
Vertical Tail Contribution
Formulas : 24   Size : 367 kb
Weight Estimation
Formulas : 17   Size : 285 kb
Wing Tail Contribution
Formulas : 15   Size : 329 kb
Wing Tail Interaction
Formulas : 12   Size : 296 kb

Contents of the Normal Shock Wave PDF

List of 35 Normal Shock Wave Formulas

Characteristic Mach Number
​Go
Characteristic Mach Number behind Shock
​Go
Critical Speed of Sound from Prandtl Relation
​Go
Density ahead of Normal Shock using Normal Shock Momentum Equation
​Go
Density behind Normal Shock given Upstream Density and Mach Number
​Go
Density behind Normal Shock using Normal Shock Momentum Equation
​Go
Density Downstream of Shock Wave using Continuity Equation
​Go
Density Ratio across Normal Shock
​Go
Density Upstream of Shock Wave using Continuity Equation
​Go
Downstream Velocity using Prandtl Relation
​Go
Enthalpy ahead of Normal Shock from Normal Shock Energy Equation
​Go
Enthalpy behind Normal Shock from Normal Shock Energy Equation
​Go
Enthalpy Difference using Hugoniot Equation
​Go
Entropy Change across Normal Shock
​Go
Flow Velocity Downstream of Shock Wave using Continuity Equation
​Go
Flow Velocity Upstream of Shock Wave using Continuity Equation
​Go
Mach Number behind Shock
​Go
Mach Number given Impact and Static Pressure
​Go
Pressure Ratio across Normal Shock
​Go
Relation between Mach Number and Characteristic Mach Number
​Go
Shock Strength
​Go
Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula
​Go
Static Enthalpy behind Normal Shock for given Upstream Enthalpy and Mach Number
​Go
Static Enthalpy Ratio across Normal Shock
​Go
Static Pressure ahead of Normal Shock using Normal Shock Momentum Equation
​Go
Static Pressure behind Normal Shock for given Upstream Pressure and Mach Number
​Go
Static Pressure behind Normal Shock using Normal Shock Momentum Equation
​Go
Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number
​Go
Temperature Ratio across Normal Shock
​Go
Upstream Velocity using Prandtl Relation
​Go
Velocity ahead of Normal Shock by Normal Shock Momentum Equation
​Go
Velocity ahead of Normal Shock from Normal Shock Energy Equation
​Go
Velocity behind Normal Shock
​Go
Velocity behind Normal Shock by Normal Shock Momentum Equation
​Go
Velocity behind Normal Shock from Normal Shock Energy Equation
​Go

Variables used in Normal Shock Wave PDF

  1. acr Critical Speed of Sound (Meter per Second)
  2. h1 Enthalpy Ahead of Normal Shock (Joule per Kilogram)
  3. h2 Enthalpy Behind Normal Shock (Joule per Kilogram)
  4. Hr Static Enthalpy Ratio Across Normal Shock
  5. M Mach Number
  6. M1 Mach Number Ahead of Normal Shock
  7. M2 Mach Number Behind Normal Shock
  8. Mcr Characteristic Mach Number
  9. M1cr Characteristic Mach Number Ahead of Shock
  10. M2cr Characteristic Mach Number Behind Shock
  11. p01 Stagnation Pressure Ahead of Normal Shock (Pascal)
  12. p02 Stagnation Pressure Behind Normal Shock (Pascal)
  13. P1 Static Pressure Ahead of Normal Shock (Pascal)
  14. P2 Static pressure Behind Normal shock (Pascal)
  15. Pr Pressure Ratio Across Normal Shock
  16. pst Static Pressure (Pascal)
  17. qc Impact Pressure (Pascal)
  18. R Specific Gas Constant (Joule per Kilogram per K)
  19. T1 Temperature Ahead of Normal Shock (Kelvin)
  20. T2 Temperature Behind Normal Shock (Kelvin)
  21. Tr Temperature Ratio Across Normal Shock
  22. uf Fluid Velocity (Meter per Second)
  23. V1 Velocity Upstream of Shock (Meter per Second)
  24. V2 Velocity Downstream of Shock (Meter per Second)
  25. γ Specific Heat Ratio
  26. ΔH Enthalpy Change (Joule per Kilogram)
  27. Δpstr Shock Strength
  28. ΔS Entropy Change (Joule per Kilogram K)
  29. ρ1 Density Ahead of Normal Shock (Kilogram per Cubic Meter)
  30. ρ2 Density Behind Normal Shock (Kilogram per Cubic Meter)
  31. ρr Density Ratio Across Normal Shock

Constants, Functions and Measurements used in Normal Shock Wave PDF

  1. 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.
  2. 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.
  3. Measurement: Temperature in Kelvin (K)
    Temperature Unit Conversion
  4. Measurement: Pressure in Pascal (Pa)
    Pressure Unit Conversion
  5. Measurement: Speed in Meter per Second (m/s)
    Speed Unit Conversion
  6. Measurement: Heat of Combustion (per Mass) in Joule per Kilogram (J/kg)
    Heat of Combustion (per Mass) Unit Conversion
  7. Measurement: Specific Heat Capacity in Joule per Kilogram per K (J/(kg*K))
    Specific Heat Capacity Unit Conversion
  8. Measurement: Density in Kilogram per Cubic Meter (kg/m³)
    Density Unit Conversion
  9. Measurement: Specific Entropy in Joule per Kilogram K (J/kg*K)
    Specific Entropy Unit Conversion
  10. Measurement: Specific Energy in Joule per Kilogram (J/kg)
    Specific Energy Unit Conversion
Download Now!
Share

Free Normal Shock Wave PDF

Get Free Normal Shock Wave PDF for Download today. Examples are included after each Formula with a link to a live Calculator! All the Formulas and Calculators support Unit Conversion as well. This PDF features 35 calculators from Aerodynamics. Inside, you'll discover a list of formulas such as Downstream Velocity using Prandtl Relation, Characteristic Mach Number and 35 more formulas!. The Variables, Functions and Constants are summarized at the end. Explore and share Normal Shock Wave PDFs!

Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Percentage calculator Fraction calculator LCM HCF Calculator
© 2016-2024 A softusvista inc. venture!


Home Icon
Home PDF Icon
FREE PDFs
🔍 Search
Category Icon
Categories
Share Icon
Share
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!