Calculator A to Z

Calculators Created by Himanshu Sharma

Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
95
Formulas Created
0
Formulas Verified
8
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 95 and verified 0 calculators across 8 different categories till date.
Aerodynamic Drag and its Reduction (21)
Created Aerodynamic force
Go
Created Ambient air density given dynamic pressure
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Created Ambient air density given gas constant
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Created Ambient air density given mach number
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Created Aspect ration in lateral plane
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Created Flat plate area
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Created Flight speed given dynamic pressure
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Created Form factor given flat plate area
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Created Gas constant given dynamic pressure
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Created Gross weight given drag
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Created Induced drag
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Created Lateral plane span given aspect ratio
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Created Lateral plane span given induced drag
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Created Mach number given gas constant
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Created Normal pressure given dynamic pressure
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Created Skin friction coefficient given flat plate area
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Created Specific heat of air given gas constant new
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Created Specific heat of air given normal pressure
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Created Temperature given gas constant
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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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3 More Aerodynamic Drag and its Reduction Calculators
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Conceptual Design (18)
Created Fuel load
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Created Fuel load from unity equation
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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 payload capability
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Created Maximum take off weight
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Created Mission fuel
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Created Mission fuel given take off, reserve and 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 Range increment of aircraft
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Created Reserve fuel
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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 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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6 More Conceptual Design Calculators
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Drag (7)
Created Coefficient of drag 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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Dynamic Pressure (7)
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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1 More Dynamic Pressure Calculators
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Lift (7)
Created Coefficient of lift given drag
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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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1 More Lift Calculators
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Mass Flow Rate (9)
Created Mass flow rate cool secondary given turbofan thrust
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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 Mass flow rate given 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 ambient air
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Created Mass flow rate of cool secondary engine
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Created Mass flow rate of turbojet thrust
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Propulsion and Engine Technology (22)
Created Area of nozzle exit of turbojet
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Created Design range given range increment
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Created Expansion velocity cool secondary given turbofan thrust
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Created Expansion velocity given thrust
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Created Expansion velocity hot primary given turbofan thrust
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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 Flight speed given thrust
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Created Gross thrust of turbojet given net thrust and ram drag
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Created Harmonic range given range increment
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Created Ideal thrust of turbojet
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Created Momentum of ambient air
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Created Net thrust of turbojet given gross thrust and ram drag
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Created Ram drag
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Created Ram drag of turbojet given gross thrust and net thrust
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Created Thrust exerted by engine
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Created Total mass flow rate through turbofan engine
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Created Turbofan thrust
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Created Turbojet gross thrust
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Created Velocity after expansion given ideal thrust
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Created Velocity of turbojet
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Weight Terminologies of Aircraft Design (4)
Created Gross 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 Zero fuel weight
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3 More Weight Terminologies of Aircraft Design Calculators
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