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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
Go
Created
Ambient air density given mach number
Go
Created
Aspect ration in lateral plane
Go
Created
Flat plate area
Go
Created
Flight speed given dynamic pressure
Go
Created
Form factor given flat plate area
Go
Created
Gas constant given dynamic pressure
Go
Created
Gross weight given drag
Go
Created
Induced drag
Go
Created
Lateral plane span given aspect ratio
Go
Created
Lateral plane span given induced drag
Go
Created
Mach number given gas constant
Go
Created
Normal pressure given dynamic pressure
Go
Created
Skin friction coefficient given flat plate area
Go
Created
Specific heat of air given gas constant new
Go
Created
Specific heat of air given normal pressure
Go
Created
Temperature given gas constant
Go
Created
Wetted area given aspect ratio
Go
Created
Wetted area given flat plate area
Go
1 More Aerodynamic Drag and its Reduction Calculators
Go
Conceptual Design
(18)
Created
Fuel load
Go
Created
Fuel load from unity equation
Go
Created
Landing weight given take off weight and mission fuel weight
Go
Created
Landing weight given zero fuel weight and reserve fuel weight
Go
Created
Maximum payload capability
Go
Created
Maximum take off weight
Go
Created
Mission fuel
Go
Created
Mission fuel given take off, reserve and zero fuel weight
Go
Created
Operating empty weight from unity equation
Go
Created
Payload of aircraft
Go
Created
Payload weight from Unity equation
Go
Created
Range increment of aircraft
Go
Created
Reserve fuel
Go
Created
Take off weight from Unity equation
Go
Created
Take off weight given reserve, mission and zero fuel weight
Go
Created
Useful load
Go
Created
Zero fuel weight given mission fuel, reserve and take off weight
Go
Created
Zero fuel weight given reserve and landing weight
Go
6 More Conceptual Design Calculators
Go
Drag
(7)
Created
Coefficient of drag given drag
Go
Created
Drag
Go
Created
Drag coefficient given lift coefficient
Go
Created
Drag coefficient new
Go
Created
Drag given aerodynamic force
Go
Created
Drag given drag coefficient
Go
Created
Drag given lift coefficient
Go
Dynamic Pressure
(7)
Created
Dynamic pressure aircraft
Go
Created
Dynamic pressure given drag coefficient
Go
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
Go
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
Go
Created
Lift given aerodynamic force
Go
Created
Lift given drag coefficient
Go
Created
Lift given induced drag
Go
Created
Lift given lift coefficient
Go
Mass Flow Rate
(9)
Created
Mass flow rate cool secondary given turbofan thrust
Go
Created
Mass flow rate given ideal thrust
Go
Created
Mass flow rate given ram drag and flight speed
Go
Created
Mass flow rate given thrust
Go
Created
Mass flow rate hot primary engine
Go
Created
Mass flow rate hot primary given turbofan thrust
Go
Created
Mass flow rate of ambient air
Go
Created
Mass flow rate of cool secondary engine
Go
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
Go
Created
Expansion velocity given thrust
Go
Created
Expansion velocity hot primary given turbofan thrust
Go
Created
Flight speed given ideal thrust
Go
Created
Flight speed given momentum of ambient air
Go
Created
Flight speed given ram drag and mass flow rate
Go
Created
Flight speed given thrust
Go
Created
Gross thrust of turbojet given net thrust and ram drag
Go
Created
Harmonic range given range increment
Go
Created
Ideal thrust of turbojet
Go
Created
Momentum of ambient air
Go
Created
Net thrust of turbojet given gross thrust and ram drag
Go
Created
Ram drag
Go
Created
Ram drag of turbojet given gross thrust and net thrust
Go
Created
Thrust exerted by engine
Go
Created
Total mass flow rate through turbofan engine
Go
Created
Turbofan thrust
Go
Created
Turbojet gross thrust
Go
Created
Velocity after expansion given ideal thrust
Go
Created
Velocity of turbojet
Go
Weight Terminologies of Aircraft Design
(4)
Created
Gross weight
Go
Created
Operating empty weight
Go
Created
Operating empty weight considering zero fuel weight
Go
Created
Zero fuel weight
Go
3 More Weight Terminologies of Aircraft Design Calculators
Go
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