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   Preliminary Aerodynamics PDF
Formulas : 17
Size : 0 kb
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Contents of the Preliminary Aerodynamics PDF

List of 17 Preliminary Aerodynamics Formulas

Aerodynamic Force
​Go
Dynamic pressure aircraft
​Go
Dynamic Pressure given Drag Coefficient
​Go
Dynamic Pressure given Gas Constant
​Go
Dynamic Pressure given Induced Drag
​Go
Dynamic Pressure given Lift Coefficient
​Go
Dynamic Pressure given Mach Number
​Go
Dynamic Pressure given Normal Pressure
​Go
Flight Speed given Dynamic Pressure
​Go
Mach Number of Moving Object
​Go
Mach Number-2
​Go
Power required at Altitude
​Go
Power required at Altitude given Power at sea-level
​Go
Power required at sea-level conditions
​Go
Velocity at Altitude
​Go
Velocity at Altitude given Velocity at Sea-Level
​Go
Velocity at Sea-Level given Lift Coefficient
​Go

Variables used in Preliminary Aerodynamics PDF

  1. a Sonic Speed (Meter per Second)
  2. bW Lateral Plane Span (Meter)
  3. c Speed of Sound (Meter per Second)
  4. CD Drag Coefficient
  5. CL Lift Coefficient
  6. cp Specific Heat of Air (Joule per Kilogram per K)
  7. Di Induced Drag (Newton)
  8. FD Drag Force (Newton)
  9. FL Lift Force (Newton)
  10. FR Aerodynamic Force (Newton)
  11. M Mach Number 2
  12. Mr Mach Number
  13. p Pressure (Pascal)
  14. PR,0 Power Required at Sea-level (Watt)
  15. PR,alt Power Required at Altitude (Watt)
  16. q Dynamic Pressure (Pascal)
  17. R Gas Constant (Joule per Kilogram per K)
  18. S Reference Area (Square Meter)
  19. T Temperature (Kelvin)
  20. v Velocity (Meter per Second)
  21. V0 Velocity at Sea-Level (Meter per Second)
  22. Valt Velocity at an Altitude (Meter per Second)
  23. Vfs Flight Speed (Meter per Second)
  24. Wbody Weight of Body (Newton)
  25. Y Heat Capacity Ratio
  26. ρ Ambient Air Density (Kilogram per Cubic Meter)
  27. ρ0 Density (Kilogram per Cubic Meter)

Constants, Functions and Measurements used in Preliminary Aerodynamics PDF

  1. Constant: pi, 3.14159265358979323846264338327950288
    Archimedes' constant
  2. Constant: [Std-Air-Density-Sea], 1.229
    Standard air density at sea-level conditions
  3. 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.
  4. Measurement: Length in Meter (m)
    Length Unit Conversion
  5. Measurement: Temperature in Kelvin (K)
    Temperature Unit Conversion
  6. Measurement: Area in Square Meter (m²)
    Area Unit Conversion
  7. Measurement: Pressure in Pascal (Pa)
    Pressure Unit Conversion
  8. Measurement: Speed in Meter per Second (m/s)
    Speed Unit Conversion
  9. Measurement: Power in Watt (W)
    Power Unit Conversion
  10. Measurement: Force in Newton (N)
    Force Unit Conversion
  11. Measurement: Specific Heat Capacity in Joule per Kilogram per K (J/(kg*K))
    Specific Heat Capacity Unit Conversion
  12. Measurement: Density in Kilogram per Cubic Meter (kg/m³)
    Density Unit Conversion
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Free Preliminary Aerodynamics PDF

Get Free Preliminary Aerodynamics 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 17 calculators from Aircraft Mechanics. Inside, you'll discover a list of formulas such as Velocity at Sea-Level given Lift Coefficient, Power required at sea-level conditions and 17 more formulas!. The Variables, Functions and Constants are summarized at the end. Explore and share Preliminary Aerodynamics PDFs!

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