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 Drag Force

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Created Drag coefficient given lift coefficient

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Created Drag Force Given Lift Coefficient

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Created Drag given aerodynamic force

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Created Drag given drag 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 given Lift Force

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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

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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 Primary Mass flow Rate in Turbofan 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