Calculators Created by Himanshu Sharma

Created Aspect Ratio of Wing

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Created Equivalent Parasite Drag Area

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Created Form Factor given Flat Plate Area

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Created Gross weight given drag

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Created Skin Friction Coefficient given Flat Plate Area

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Created Span given Aspect Ratio

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Created Span given Induced Drag

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Created Wetted Area given Aspect Ratio

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Created Wetted Area given Flat Plate Area

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4 More Aerodynamic Design Calculators

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Created Ambient air density given dynamic pressure

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Created Ambient air density given mach number

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Created Ambient Air Density given Mach Number and Temperature

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Created Ambient Pressure given Dynamic Pressure and Mach Number

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Created Gas constant given dynamic pressure

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Created Mach Number given Dynamic Pressure

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Created Mach Number given Static and Dynamic Pressure

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Created Temperature given Dynamic Pressure and Mach Number

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6 More Atmosphere and Gas Properties Calculators

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Created Fuel load

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Created Maximum payload capability

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Created Mission fuel

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Created Range increment of aircraft

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Created Reserve fuel

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14 More Design Process Calculators

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Created Coefficient of drag given drag

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Created Coefficient of lift given drag

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Created Drag

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Created Drag coefficient given lift coefficient

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Created Drag coefficient new

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Created Drag given aerodynamic force

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Created Drag given drag coefficient

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Created Drag given lift coefficient

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Created Induced Drag for Wings having Elliptic Lift Distribution

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Created Lift coefficient given drag coefficient

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Created Lift coefficient new

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Created Lift given aerodynamic force

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Created Lift given drag coefficient

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Created Lift given induced drag

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Created Lift given lift coefficient

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6 More Lift and Drag Polar Calculators

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Created Aerodynamic force

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Created Dynamic pressure aircraft

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Created Dynamic pressure given drag coefficient

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Created Dynamic pressure given gas constant

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Created Dynamic pressure given induced drag

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Created Dynamic pressure given lift coefficient

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Created Dynamic pressure given mach number

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Created Dynamic pressure given normal pressure

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Created Flight speed given dynamic pressure

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8 More Preliminary Aerodynamics Calculators

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Created Design range given range increment

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Created Harmonic range given range increment

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25 More Preliminary Design Calculators

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Created Flight Speed given Ideal Thrust

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Created Flight Speed given Momentum of Ambient Air

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Created Flight Speed given Ram Drag and Mass Flow Rate

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Created Ideal Thrust of Jet Engine

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Created Mass Flow given Momentum in Ambient Air

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Created Mass Flow Rate given Ideal Thrust

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Created Mass Flow Rate given Ram Drag and Flight Speed

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Created Momentum of Ambient Air

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Created Ram drag

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Created Velocity after Expansion given Ideal Thrust

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11 More Thrust Generation Calculators

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Created Bypass Exhaust Velocity given Turbofan Thrust

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Created Bypass Mass Flow Rate given Turbofan Thrust

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Created Core Exhaust Velocity given Turbofan Thrust

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Created Mass flow rate hot primary engine

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Created Mass flow rate hot primary given turbofan thrust

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Created Mass flow rate of cool secondary engine

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Created Total mass flow rate through turbofan engine

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Created Turbofan thrust

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2 More Turbofans Calculators

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Created Exhaust Velocity given Gross Thrust in Turbojet

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Created Exhaust Velocity given Thrust in Turbojet

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Created Flight Speed given Thrust in Turbojet

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Created Gross Thrust of Turbojet given Net Thrust

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Created Mass Flow Rate in Turbojet given Thrust

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Created Mass Flow Rate of Turbojet given Gross Thrust

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Created Net Thrust of Turbojet given Gross Thrust

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Created Net Thrust Produced by Turbojet

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Created Nozzle Exit Area in Turbojet

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Created Ram Drag of Turbojet given Gross Thrust

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Created Turbojet Gross Thrust

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3 More Turbojets Calculators

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Created Fuel load from unity equation

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Created Gross weight

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Created Landing weight given take off weight and mission fuel weight

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Created Landing weight given zero fuel weight and reserve fuel weight

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Created Maximum take off weight

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Created Mission fuel given take off, reserve and zero fuel weight

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Created Operating empty weight

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Created Operating empty weight considering zero fuel weight

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Created Operating empty weight from unity equation

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Created Payload of aircraft

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Created Payload weight from Unity equation

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Created Take off weight from Unity equation

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Created Take off weight given reserve, mission and zero fuel weight

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Created Useful load

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Created Zero fuel weight

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Created Zero fuel weight given mission fuel, reserve and take off weight

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Created Zero fuel weight given reserve and landing weight

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List of Calculators by Himanshu Sharma