Calculators Created by Himanshu Sharma

National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
94
Formulas Created
0
Formulas Verified
10
Across Categories

List of Calculators by Himanshu Sharma

Following is a combined list of all the calculators that have been created and verified by Himanshu Sharma. Himanshu Sharma has created 94 and verified 0 calculators across 10 different categories till date.
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 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 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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