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Calculators Created by Himanshu Sharma
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.
Aerodynamic Design
(9)
Created
Aspect Ratio of Wing
Go
Created
Equivalent Parasite Drag Area
Go
Created
Form Factor given Flat Plate Area
Go
Created
Gross Weight given Drag
Go
Created
Skin Friction Coefficient given Flat Plate Area
Go
Created
Span given Aspect Ratio
Go
Created
Span given Induced Drag
Go
Created
Wetted Area given Aspect Ratio
Go
Created
Wetted Area given Flat Plate Area
Go
4 More Aerodynamic Design Calculators
Go
Atmosphere and Gas Properties
(8)
Created
Ambient air density given dynamic pressure
Go
Created
Ambient air density given mach number
Go
Created
Ambient Air Density given Mach Number and Temperature
Go
Created
Ambient Pressure given Dynamic Pressure and Mach Number
Go
Created
Gas constant given dynamic pressure
Go
Created
Mach Number given Dynamic Pressure
Go
Created
Mach Number given Static and Dynamic Pressure
Go
Created
Temperature given Dynamic Pressure and Mach Number
Go
6 More Atmosphere and Gas Properties Calculators
Go
Design Process
(5)
Created
Fuel Load
Go
Created
Maximum Payload Capability
Go
Created
Mission Fuel
Go
Created
Range Increment of Aircraft
Go
Created
Reserve Fuel
Go
14 More Design Process Calculators
Go
Lift and Drag Polar
(15)
Created
Coefficient of drag given drag
Go
Created
Coefficient of lift given drag
Go
Created
Drag
Go
Created
Drag coefficient given lift coefficient
Go
Created
Drag coefficient new
Go
Created
Drag Force Given Lift Coefficient
Go
Created
Drag given aerodynamic force
Go
Created
Drag given drag coefficient
Go
Created
Induced Drag for Wings having Elliptic Lift Distribution
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
6 More Lift and Drag Polar Calculators
Go
Preliminary Aerodynamics
(9)
Created
Aerodynamic force
Go
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
Created
Flight speed given dynamic pressure
Go
8 More Preliminary Aerodynamics Calculators
Go
Preliminary Design
(2)
Created
Design Range given Range Increment
Go
Created
Harmonic Range given Range Increment
Go
25 More Preliminary Design Calculators
Go
Thrust Generation
(10)
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
Ideal Thrust of Jet Engine
Go
Created
Mass Flow given Momentum in Ambient Air
Go
Created
Mass Flow Rate given Ideal Thrust
Go
Created
Mass Flow Rate given Ram Drag and Flight Speed
Go
Created
Momentum of Ambient Air
Go
Created
Ram drag
Go
Created
Velocity after Expansion given Ideal Thrust
Go
11 More Thrust Generation Calculators
Go
Turbofans
(8)
Created
Bypass Exhaust Velocity given Turbofan Thrust
Go
Created
Bypass Mass Flow Rate given Turbofan Thrust
Go
Created
Core Exhaust Velocity given Turbofan 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 cool secondary engine
Go
Created
Total mass flow rate through turbofan engine
Go
Created
Turbofan thrust
Go
2 More Turbofans Calculators
Go
Turbojets
(11)
Created
Exhaust Velocity given Gross Thrust in Turbojet
Go
Created
Exhaust Velocity given Thrust in Turbojet
Go
Created
Flight Speed given Thrust in Turbojet
Go
Created
Gross Thrust of Turbojet given Net Thrust
Go
Created
Mass Flow Rate in Turbojet given Thrust
Go
Created
Mass Flow Rate of Turbojet given Gross Thrust
Go
Created
Net Thrust of Turbojet given Gross Thrust
Go
Created
Net Thrust Produced by Turbojet
Go
Created
Nozzle Exit Area in Turbojet
Go
Created
Ram Drag of Turbojet given Gross Thrust
Go
Created
Turbojet Gross Thrust
Go
3 More Turbojets Calculators
Go
Weight Estimation
(17)
Created
Fuel Load from Unity Equation
Go
Created
Gross weight
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 take off weight
Go
Created
Mission Fuel given Take Off, Reserve and Zero Fuel Weight
Go
Created
Operating Empty Weight
Go
Created
Operating Empty Weight considering 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
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
Go
Created
Zero Fuel Weight given Mission Fuel, Reserve and Take Off Weight
Go
Created
Zero Fuel Weight given Reserve and Landing Weight
Go
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