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
Go
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
Go
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
Go
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
Go
1 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
Go
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
Go
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
Go
Created Dynamic pressure given induced drag
Go
Created Dynamic pressure given lift coefficient
Go
Created Dynamic pressure given mach number
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Created Dynamic pressure given normal pressure
Go
Lift (7)
Created Coefficient of lift given drag
Go
Created Lift coefficient given drag coefficient
Go
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
Go
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
Go
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
Go
Propulsion and Engine Technology (22)
Created Area of nozzle exit of turbojet
Go
Created Design range given range increment
Go
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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