Calculator A to Z
🔍
Chemistry
Engineering
Financial
Health
Math
Physics
Playground
Calculators Created by Shikha Maurya
Shikha Maurya
Indian Institute of Technology
(IIT)
,
Bombay
https://www.linkedin.com/in/shikha-maurya-eager-to-learn/
108
Formulas Created
170
Formulas Verified
68
Across Categories
List of Calculators by Shikha Maurya
Following is a combined list of all the calculators that have been created and verified by Shikha Maurya. Shikha Maurya has created 108 and verified 170 calculators across 68 different categories till date.
Aerodynamic Nomenclature
(8)
Verified
Aerodynamic axial force
Go
Verified
Aerodynamic normal force
Go
Verified
Aerodynamic side force
Go
Verified
Angle of attack
Go
Verified
Pitching moment
Go
Verified
Pitching moment coefficient
Go
Verified
Side force coefficient
Go
Verified
Sideslip angle
Go
9 More Aerodynamic Nomenclature Calculators
Go
Altitude Effects on Power Required and Available
(3)
Verified
Power required at sea-level condition
Go
Verified
Velocity at an altitude for given velocity at sea-level condition
Go
Verified
Velocity at sea-level condition
Go
3 More Altitude Effects on Power Required and Available Calculators
Go
Basic Compressible Flow
(3)
Created
Critical Density
Go
Created
Critical Pressure
Go
Created
Critical Temperature
Go
3 More Basic Compressible Flow Calculators
Go
Basics
(1)
Created
Isentropic compressibility for given density and speed of sound
Go
6 More Basics Calculators
Go
Bending Stresses
(1)
Verified
Section Modulus of Steel Beam when Stress in Steel for Unshored Members is Given
Go
9 More Bending Stresses Calculators
Go
Blast-wave part 2
(3)
Verified
Pressure coefficient combined with blast wave for the shuttle
Go
Verified
Pressure coefficient combined with blast wave for the shuttle at angle of attack
Go
Verified
Pressure coefficient for Blunt-nosed cylinder:
Go
3 More Blast-wave part 2 Calculators
Go
Bodies connected by string and passing over smooth pulley
(3)
Verified
Acceleration of bodies
Go
Verified
Mass of body B of smaller mass
Go
Verified
Tension in the string if both the bodies are freely hanging
Go
Bodies connected by string, one hanging free, other lying on rough horizontal plane
(1)
Verified
Acceleration of system with bodies one hanging free and other lying on rough horizontal plane
Go
1 More Bodies connected by string, one hanging free, other lying on rough horizontal plane Calculators
Go
Bodies connected by string, one hanging free, other lying on smooth horizontal plane
(2)
Verified
Acceleration in system
Go
Verified
Tension in string if only one body is freely suspended
Go
Boundary layer flow
(4)
Verified
Drag force on the plate in boundary layer flow
Go
Verified
Reynold number for drag force on the plate in boundary layer flow
Go
Verified
Viscosity of liquid for drag force on the plate in boundary layer flow
Go
Verified
Width of the plate for drag force on the plate in boundary layer flow
Go
17 More Boundary layer flow Calculators
Go
Boundary-Layer Equations for Hypersonic Flow: Self-Similar Solutions
(5)
Verified
Adiabatic wall enthalpy using Stanton number
Go
Verified
Enthalpy of wall using Stanton number
Go
Verified
Nusselt number for hypersonic vehicle
Go
Verified
Reynolds number for given Nusselt's number, Stanton number and Prandtl number
Go
Verified
Skin friction coefficient for incompressible flow
Go
15 More Boundary-Layer Equations for Hypersonic Flow: Self-Similar Solutions Calculators
Go
Circulation
(1)
Verified
Circulation developed on the airfoil
Go
3 More Circulation Calculators
Go
Coefficient's
(1)
Verified
Lift coefficient for lift force in body moving on fluid
Go
5 More Coefficient's Calculators
Go
Compressible flow
(2)
Verified
Mach angle for the compressible fluid flow
Go
Verified
Velocity of fluid considering the Mach angle in the compressible fluid flow
Go
11 More Compressible flow Calculators
Go
Contribution of Aircraft Components- Part 1
(4)
Verified
Moment produced by vertical tail for given side force
Go
Verified
Vertical tail angle of attack
Go
Verified
Vertical tail moment arm for given side force
Go
Verified
Vertical tail side force for given moment
Go
11 More Contribution of Aircraft Components- Part 1 Calculators
Go
Contribution of Aircraft Components- Part 2
(2)
Verified
Moment produced by vertical tail for given moment coefficient
Go
Verified
Yawing moment coefficient when wingspan is given
Go
12 More Contribution of Aircraft Components- Part 2 Calculators
Go
Contribution of Aircraft Components- Part 3
(5)
Verified
Vertical tail area for given vertical tail volume ratio
Go
Verified
Vertical tail moment arm for given vertical tail volume ratio
Go
Verified
Vertical tail volume ratio
Go
Verified
Wing area for given vertical tail volume ratio
Go
Verified
Wingspan for given vertical tail volume ratio
Go
10 More Contribution of Aircraft Components- Part 3 Calculators
Go
Cutting Force
(3)
Created
Cutting force for given force along shear force, shear,friction & normal rake angles
Go
Created
Cutting force for given resultant force in merchant circle, friction angle and normal rake angle
Go
Created
Cutting force for shear stress,width of cut,uncut chip thickness,friction,normal rake & shear angles
Go
3 More Cutting Force Calculators
Go
Discharge
(4)
Verified
Discharge over rectangle weir considering Bazin's formula
Go
Verified
Discharge over rectangle weir considering Francis's formula
Go
Verified
Discharge with velocity of approach
Go
Verified
Discharge without velocity of approach
Go
9 More Discharge Calculators
Go
Dynamics of fluid flow
(2)
Verified
Coefficient of pitot-tube for velocity at any point
Go
Verified
Resultant bend force along x and y direction
Go
4 More Dynamics of fluid flow Calculators
Go
Elevator Hinge Moment
(1)
Verified
Elevator chord length for given hinge moment coefficient
Go
4 More Elevator Hinge Moment Calculators
Go
Flat-Plate for Viscous flow case
(1)
Verified
Total enthalpy in the inviscid flow outside the boundary layer
Go
14 More Flat-Plate for Viscous flow case Calculators
Go
Flight Envelope
(5)
Verified
Lift Coefficient for given turn rate
Go
Verified
Load factor for given turn rate for a high-performance fighter aircraft
Go
Verified
Radius of turn for given lift coefficient
Go
Verified
Radius of turn for given wing loading
Go
Verified
Turn rate for given wing loading
Go
10 More Flight Envelope Calculators
Go
Flow through pipes
(7)
Verified
Area of the nozzle at outlet for maximum power transmission through nozzle
Go
Verified
Area of the pipe for maximum power transmission through nozzle
Go
Verified
Diameter of nozzle for maximum power transmission through nozzle
Go
Verified
Diameter of the equivalent pipe
Go
Verified
Discharge in the equivalent pipe
Go
Verified
Length of pipe for maximum power transmission through nozzle
Go
Verified
Length of the equivalent pipe
Go
14 More Flow through pipes Calculators
Go
Force Along The Shear
(1)
Created
Force along shear force for given R of merchant circle, shear, friction and normal rake angles
Go
2 More Force Along The Shear Calculators
Go
Forces on sub-merged bodies
(6)
Verified
Angle of attack for circulation developed on the airfoil
Go
Verified
Area of the body for lift force in body moving on fluid
Go
Verified
Chord length for circulation developed on the airfoil
Go
Verified
Lift force for a body moving in a fluid of certain density
Go
Verified
Pressure drag from total drag force on a sphere
Go
Verified
Skin friction drag from total drag force on a sphere
Go
21 More Forces on sub-merged bodies Calculators
Go
Fundamentals of Inviscid Incompressible flow
(15)
Created
2-D Lift coefficient for cylinder
Go
Created
Airspeed measurement by Pitot tube for low-speed incompressible flow
Go
Created
Airspeed measurement by venturi
Go
Created
Circulation by Kutta-Joukowski theorem
Go
Created
Freestream density by Kutta-Joukowski theorem
Go
Created
Freestream velocity by Kutta-Joukowski theorem
Go
Created
Height difference of manometric fluid for given pressure difference
Go
Created
Lift per unit span by Kutta-Joukowski theorem
Go
Created
Location of stagnation point outside cylinder for lifting flow
Go
Created
Radius of cylinder for non-lifting flow
Go
Created
Source Strength for 2-D incompressible source flow
Go
Created
Stagnation streamline equation for flow over semi-infinite body
Go
Created
Test section velocity for low speed wind tunnel in terms of height difference of manometric fluid
Go
Created
Test section velocity in low-speed wind tunnel
Go
Created
Velocity at a point on airfoil for given pressure coefficient and free-stream velocity
Go
Hypersonic Equivalence Principle and Blast-Wave Theory
(3)
Verified
Modified pressure equation for cylindrical blast wave
Go
Verified
Pressure ratio for blunt cylinder blast wave
Go
Verified
Pressure ratio for blunt slab blast wave
Go
13 More Hypersonic Equivalence Principle and Blast-Wave Theory Calculators
Go
Hypersonic Flight Paths: Velocity-Altitude Map
(1)
Verified
Blunt-nosed radial coordinate flat plate (first approximation):
Go
8 More Hypersonic Flight Paths: Velocity-Altitude Map Calculators
Go
Hypersonic Inviscid Flowfields: Exact Methods
(7)
Verified
Density before shock formation for compression wave
Go
Verified
Local shock velocity equation
Go
Verified
Mach wave behind the shock
Go
Verified
Mach wave behind the shock with mach infinity
Go
Verified
New pressure after the shock formation, subtracted to velocity for expansion wave
Go
Verified
Pressure ratio for unsteady waves with subtracted induced mass motion for expansion waves
Go
Verified
Temperature ratio for unsteady compression waves
Go
11 More Hypersonic Inviscid Flowfields: Exact Methods Calculators
Go
Ideal flow or Potential flow
(1)
Verified
Distance of stagnation point S from source in flow past a half body
Go
14 More Ideal flow or Potential flow Calculators
Go
Incompressible flow over airfoil
(8)
Created
Boundary layer thickness for laminar flow
Go
Created
Boundary layer thickness for Turbulent flow
Go
Created
Center of pressure location for cambered airfoil
Go
Created
Lift coefficient for cambered airfoil
Go
Created
Lift coefficient for symmetrical airfoil by Thin airfoil theory
Go
Created
Moment coefficient about leading-edge for symmetrical airfoil by thin airfoil theory
Go
Created
Skin friction drag coefficient for flat plate in laminar flow
Go
Created
Skin friction drag coefficient for flat plate in Turbulent flow
Go
Landing Performance
(1)
Verified
Stall velocity for given touchdown velocity
Go
4 More Landing Performance Calculators
Go
Length of Weir
(4)
Verified
Length of weir considering Bazin's formula without velocity approach
Go
Verified
Length of weir considering Francis's formula
Go
Verified
Length of weir or notch for velocity of approach
Go
Verified
Length of weir or notch without velocity of approach
Go
4 More Length of Weir Calculators
Go
Loss of Head
(1)
Verified
Loss of pressure head for viscous flow between two parallel plates
Go
2 More Loss of Head Calculators
Go
Loss of Head
(2)
Verified
Loss of head at entrance of pipe
Go
Verified
Loss of head in equivalent pipe
Go
6 More Loss of Head Calculators
Go
Maneuvering Flight
(1)
Verified
Velocity for a given pull-down maneuver radius
Go
11 More Maneuvering Flight Calculators
Go
Merchant Force Circle (Mechanics of Orthogonal metal cutting)
(8)
Created
Friction angle for given R of merchant circle, force along shear, shear, and normal rake angle
Go
Created
Normal rake angle for given Resultant force, force along shear, shear, and friction angle
Go
Created
R in merchant circle for given force along the shear force, shear, friction & normal rake angles
Go
Created
Resultant force in merchant circle for given cutting force, friction and normal rake angles
Go
Created
Shear angle for given Resultant force, force along shear force, friction, and normal rake angles
Go
Created
Shear stress for cutting force,width of cut,uncut chip thickness,friction,normal rake & shear angles
Go
Created
Uncut chip thickness for cutting force,shear stress,width of cut,friction,normal rake & shear angles
Go
Created
Width of cut for cutting force,shear stress,uncut chip thickness,friction,normal rake & shear angles
Go
14 More Merchant Force Circle (Mechanics of Orthogonal metal cutting) Calculators
Go
Normal Shock Waves
(21)
Created
Critical speed of sound from Prandtl relation
Go
Created
Density ahead of normal shock using normal shock momentum equation
Go
Created
Density behind normal shock for given upstream density and Mach number
Go
Created
Density behind normal shock using normal shock momentum equation
Go
Created
Density ratio across a normal shock
Go
Created
Enthalpy ahead of normal shock from normal shock energy equation
Go
Created
Enthalpy behind of normal shock from normal shock energy equation
Go
Created
Pressure ratio across a normal shock
Go
Created
Stagnation pressure behind normal shock by Rayleigh Pitot tube formula
Go
Created
Static enthalpy behind normal shock for given upstream enthalpy and Mach number
Go
Created
Static enthalpy ratio across normal shock
Go
Created
Static Pressure ahead of normal shock using normal shock momentum equation
Go
Created
Static pressure behind normal shock for given upstream pressure and Mach number
Go
Created
Static Pressure behind of normal shock using normal shock momentum equation
Go
Created
Static temperature behind normal shock for given upstream temperature and Mach number
Go
Created
Temperature ratio across a normal shock
Go
Created
Velocity ahead of normal shock by normal shock momentum equation
Go
Created
Velocity ahead of normal shock from normal shock energy equation
Go
Created
Velocity behind of normal shock by normal shock momentum equation
Go
Created
Velocity behind of normal shock from normal shock energy equation
Go
Created
Velocity upstream of shock using Prandtl relation
Go
8 More Normal Shock Waves Calculators
Go
Number of Connectors in Bridges
(5)
Verified
Effective Concrete Area when Force in Slab is Given
Go
Verified
Force in Slab at Maximum Positive Moments when Minimum Number of Connectors for Bridges is Given
Go
Verified
Force in Slab when Effective Concrete Area is Given
Go
Verified
Minimum Number of Connectors for Bridges
Go
Verified
Steel Yield Strength when Total Area of Steel Section is Given
Go
13 More Number of Connectors in Bridges Calculators
Go
Oblique Shock and Expansion Waves
(16)
Created
Component of downstream Mach number normal to oblique shock for given normal upstream Mach number
Go
Created
Density behind oblique shock for given upstream density and normal upstream Mach number
Go
Created
Density ratio across the oblique shock
Go
Created
Flow deflection angle in terms of Prandtl Meyer function
Go
Created
Forward Mach angle of expansion fan
Go
Created
Prandtl Meyer function
Go
Created
Prandtl Meyer function at upstream Mach number
Go
Created
Pressure behind expansion fan
Go
Created
Pressure behind oblique shock for given upstream pressure and normal upstream Mach number
Go
Created
Pressure ratio across the expansion fan
Go
Created
Pressure ratio across the oblique shock
Go
Created
Rearward Mach angle of the expansion fan
Go
Created
Temperature behind expansion fan
Go
Created
Temperature behind oblique shock for given upstream temperature and normal upstream Mach number
Go
Created
Temperature ratio across the expansion fan
Go
Created
Temperature ratio across the oblique shock
Go
3 More Oblique Shock and Expansion Waves Calculators
Go
Power Absorbed
(1)
Verified
Power absorbed in overcoming viscous resistance in journal bearing
Go
2 More Power Absorbed Calculators
Go
Power Transmission Efficiency
(2)
Verified
Efficiency of power transmission through nozzle for velocity and total head
Go
Verified
Efficiency of power transmission through the nozzle
Go
1 More Power Transmission Efficiency Calculators
Go
Pressure
(12)
Created
Dynamic pressure in incompressible flow
Go
Created
Pressure at downstream point on streamline by Bernoulli's equation
Go
Created
Pressure at upstream point on streamline by Bernoulli's equation
Go
Created
Pressure Coefficient
Go
Created
Pressure coefficient in terms of velocity ratio for incompressible flow
Go
Created
Pressure difference in low-speed wind tunnel for given test section velocity
Go
Created
Pressure difference measured by manometer in low-speed wind tunnel
Go
Created
Static pressure in incompressible flow
Go
Created
Surface pressure coefficient for lifting flow over circular cylinder
Go
Created
Surface pressure coefficient for non-lifting flow over circular cylinder
Go
Created
Surface pressure on body in terms of Pressure coefficient
Go
Created
Total pressure in incompressible flow
Go
Radial Velocity
(3)
Created
Radial velocity for 2-D incompressible source flow
Go
Created
Radial velocity for lifting flow over circular cylinder
Go
Created
Radial velocity for non-lifting flow over circular cylinder
Go
Rate of Climb
(2)
Verified
Excess power
Go
Verified
Total Drag for given excess power
Go
8 More Rate of Climb Calculators
Go
Reference Temperature Method
(1)
Verified
Overall skin-friction drag coefficient
Go
14 More Reference Temperature Method Calculators
Go
Relationship between Stick Force and Hinge Moment
(5)
Verified
Elevator deflection angle for given stick force
Go
Verified
Elevator Stick Force
Go
Verified
Elevator stick force for given hinge moment coefficient
Go
Verified
Gearing ratio for given stick force
Go
Verified
Stick deflection angle for given gearing ratio
Go
13 More Relationship between Stick Force and Hinge Moment Calculators
Go
Rotational Speed
(1)
Verified
Rotational speed considering power absorbed and torque in journal bearing
Go
2 More Rotational Speed Calculators
Go
Shear Range
(1)
Verified
Horizontal Shear Range at the juncture of Slab and Beam
Go
11 More Shear Range Calculators
Go
Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations
(3)
Verified
Enthalpy equation using coefficient of pressure for calorically perfect gas
Go
Verified
Free stream enthalpy
Go
Verified
Total specific enthalpy
Go
8 More Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations Calculators
Go
Stream Function
(9)
Created
Stream function for 2-D Doublet flow
Go
Created
Stream function for 2-D incompressible source flow
Go
Created
Stream function for 2-D Vortex flow
Go
Created
Stream function for flow over Rankine oval
Go
Created
Stream function for lifting flow over a circular cylinder
Go
Created
Stream function for non-lifting flow over a circular cylinder
Go
Created
Stream function for semi-infinite body
Go
Created
Stream function for uniform incompressible flow
Go
Created
Stream function for uniform incompressible flow in polar coordinates
Go
Tail Contribution
(5)
Verified
Angle of attack at the tail
Go
Verified
Downwash angle
Go
Verified
Pitching moment due to tail
Go
Verified
Tail Pitching moment for given moment coefficient
Go
Verified
Total Lift Coefficient of wing-tail combination
Go
16 More Tail Contribution Calculators
Go
Tail Contribution Contd
(5)
Verified
Horizontal tail area for given tail volume ratio
Go
Verified
Horizontal tail volume ratio
Go
Verified
Tail moment arm for given horizontal tail volume ratio
Go
Verified
Wing Mean aerodynamic chord for given horizontal tail volume ratio
Go
Verified
Wing Reference area for given horizontal tail volume ratio
Go
9 More Tail Contribution Contd Calculators
Go
Takeoff Performance
(10)
Verified
Coefficient of rolling friction during ground roll
Go
Verified
Drag during ground effect
Go
Verified
Ground effect factor
Go
Verified
Lift acting on aircraft during ground roll
Go
Verified
Liftoff distance
Go
Verified
Maximum Lift coefficient for given liftoff velocity
Go
Verified
Resistance force during ground roll
Go
Verified
Stall velocity for given weight
Go
Verified
Thrust for given liftoff distance
Go
Verified
Weight of aircraft during ground roll
Go
4 More Takeoff Performance Calculators
Go
Tangential Velocity
(3)
Created
Tangential velocity for 2-D Vortex flow
Go
Created
Tangential velocity for lifting flow over circular cylinder
Go
Created
Tangential velocity for non-lifting flow over circular cylinder
Go
The Atmosphere
(5)
Verified
Absolute altitude
Go
Verified
Geometric altitude
Go
Verified
Geometric altitude for given geopotential altitude
Go
Verified
Geopotential altitude
Go
Verified
Lapse rate
Go
Torque Required
(2)
Verified
Torque required considering power absorbed in journal bearing
Go
Verified
Torque required to overcome the shear force in journal bearing
Go
3 More Torque Required Calculators
Go
Turbulent flow
(3)
Verified
Average height of irregularities for turbulent flow in pipes
Go
Verified
Power required to maintain the turbulent flow
Go
Verified
Roughness Reynold number for turbulent flow in pipes
Go
15 More Turbulent flow Calculators
Go
Turning Flight
(7)
Verified
Bank angle during level turn
Go
Verified
Load factor for a given turn radius
Go
Verified
Load factor given Lift Force and Weight
Go
Verified
Turn rate
Go
Verified
Velocity for a given turn radius
Go
Verified
Velocity for a given turn rate
Go
Verified
Weight for a given load factor
Go
5 More Turning Flight Calculators
Go
Ultimate Shear Strength of Connectors in Bridges
(3)
Verified
Channel Web Thickness when Ultimate Shear Connector Strength for Channels is Given
Go
Verified
Elastic Modulus of Concrete given Ultimate Shear Connector Strength for Welded Studs
Go
Verified
Ultimate Shear Strength for Welded Studs
Go
6 More Ultimate Shear Strength of Connectors in Bridges Calculators
Go
Velocity
(1)
Verified
Velocity of airfoil for circulation developed on the airfoil
Go
5 More Velocity Calculators
Go
Velocity of Flow
(3)
Verified
Velocity of flow at the outlet of the nozzle
Go
Verified
Velocity of flow at the outlet of the nozzle for efficiency and head
Go
Verified
Velocity of fluid in pipe for head loss at the entrance of a pipe
Go
6 More Velocity of Flow Calculators
Go
Velocity of Sound Wave
(1)
Verified
Velocity of sound wave considering Mach angle in the compressible fluid flow
Go
4 More Velocity of Sound Wave Calculators
Go
Velocity Potential
(5)
Created
Velocity potential for 2-D doublet flow
Go
Created
Velocity potential for 2-D source flow
Go
Created
Velocity potential for 2-D Vortex flow
Go
Created
Velocity potential for uniform incompressible flow
Go
Created
Velocity potential for uniform incompressible flow in polar coordinates
Go
Viscosity of Fluid
(1)
Verified
Viscosity of fluid or oil for capillary tube method
Go
3 More Viscosity of Fluid Calculators
Go
Viscous flow
(8)
Verified
Diameter of capillary tube
Go
Verified
Difference of pressure for viscous flow between two parallel plates
Go
Verified
Discharge in capillary tube method
Go
Verified
Length for difference of pressure in viscous flow between two parallel plates
Go
Verified
Length for pressure head loss in viscous flow between two parallel plates
Go
Verified
Length of tube in capillary tube method
Go
Verified
Shear force for torque and diameter of shaft in journal bearing
Go
Verified
Shear stress in the fluid or oil of journal bearing
Go
12 More Viscous flow Calculators
Go
Viscous Flow: Basic Aspects, Boundary Layer Results, and Aerodynamic Heating
(3)
Verified
Non dimensional internal energy parameter using wall-to-freestream temperature ratio
Go
Verified
Non dimensional static enthalpy
Go
Verified
Stanton equation using Overall skin friction coefficient for incompressible flow
Go
13 More Viscous Flow: Basic Aspects, Boundary Layer Results, and Aerodynamic Heating Calculators
Go
Share
Facebook
Twitter
WhatsApp
Reddit
LinkedIn
E-Mail
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!