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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
73
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 73 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
Airfoil
(3)
Verified
Angle of Attack for Circulation developed on Airfoil
Go
Verified
Chord Length for Circulation developed on Airfoil
Go
Verified
Circulation developed on Airfoil
Go
2 More Airfoil Calculators
Go
Altitude Effects on Power Required and Available
(3)
Verified
Power required at sea-level conditions
Go
Verified
Velocity at Altitude given Velocity at Sea-Level
Go
Verified
Velocity at sea-level condition
Go
4 More Altitude Effects on Power Required and Available Calculators
Go
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
Basic Aspects, Boundary Layer Results, and Aerodynamic Heating of Viscous Flow
(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 Basic Aspects, Boundary Layer Results, and Aerodynamic Heating of Viscous Flow 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
Basic Formulas
(3)
Verified
Area of Nozzle at Outlet for Maximum Power Transmission through Nozzle
Go
Verified
Area of Pipe for Maximum Power Transmission through Nozzle
Go
Verified
Discharge in Equivalent Pipe
Go
9 More Basic Formulas Calculators
Go
Basics
(1)
Created
Isentropic compressibility for given density and speed of sound
Go
7 More Basics Calculators
Go
Bending Stresses
(1)
Verified
Section Modulus of Steel Beam given Stress in Steel for Unshored Members
Go
9 More Bending Stresses Calculators
Go
Blast-wave part 2
(3)
Verified
Pressure coefficient combined with blast wave for shuttle
Go
Verified
Pressure coefficient combined with blast wave for 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 String if both 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 Plate in Boundary Layer Flow
Go
Verified
Reynold number for Drag Force on Plate in Boundary Layer Flow
Go
Verified
Viscosity of Liquid for Drag Force on Plate in Boundary Layer Flow
Go
Verified
Width of Plate for Drag Force on 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
Coefficient's
(1)
Verified
Lift coefficient for lift force in body moving on fluid
Go
4 More Coefficient's Calculators
Go
Compressible Flow
(2)
Verified
Mach angle for Compressible Fluid Flow
Go
Verified
Velocity of projectile of mach cone in compressible fluid flow
Go
5 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 using Wingspan
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 and 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, rake and shear angles
Go
3 More Cutting Force Calculators
Go
Diameter and Length of Pipe
(4)
Verified
Diameter of Equivalent Pipe
Go
Verified
Diameter of nozzle for maximum power transmission through nozzle
Go
Verified
Length of Equivalent Pipe
Go
Verified
Length of pipe for maximum power transmission through nozzle
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
Drag Force on Body
(2)
Verified
Pressure Drag from Total Drag Force on Sphere
Go
Verified
Skin Friction Drag from Total Drag Force on Sphere
Go
5 More Drag Force on Body 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
5 More Dynamics of Fluid Flow Calculators
Go
Elevator and Stick Deflection Angles
(2)
Verified
Elevator deflection angle for given stick force
Go
Verified
Stick deflection angle for given gearing ratio
Go
2 More Elevator and Stick Deflection Angles Calculators
Go
Enthalpy and Velocity
(9)
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
Static enthalpy behind normal shock for given upstream enthalpy and Mach number
Go
Created
Static enthalpy ratio across 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
2 More Enthalpy and Velocity Calculators
Go
Flight Envelope
(5)
Verified
Lift Coefficient for given turn rate
Go
Verified
Load factor for given turn rate for 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
11 More Flight Envelope Calculators
Go
Force Along Shear
(1)
Created
Force along shear force for given R of merchant circle, shear, friction, and normal rake angles
Go
2 More Force Along Shear Calculators
Go
Gearing Ratio
(1)
Verified
Gearing ratio for given stick force
Go
3 More Gearing Ratio Calculators
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 shock
Go
Verified
Mach wave behind shock with mach infinity
Go
Verified
New pressure after 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 half body
Go
13 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
Introduction
(8)
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
Radius of capillary tube
Go
Verified
Shear force for torque and diameter of shaft in journal bearing
Go
Verified
Shear Stress in Fluid or Oil of Journal Bearing
Go
11 More Introduction Calculators
Go
Introduction
(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 given Height difference of Manometric Fluid
Go
Created
Test section Velocity in Low-Speed Wind Tunnel
Go
Created
Velocity at point on Airfoil for given Pressure Coefficient and Free-stream Velocity
Go
1 More Introduction Calculators
Go
Landing Performance
(1)
Verified
Stall velocity for given touchdown velocity
Go
3 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
Lift Force on Body
(2)
Verified
Area of body for Lift Force in body moving on Fluid
Go
Verified
Lift Force for body moving in Fluid of Certain Density
Go
5 More Lift Force on Body Calculators
Go
Longitudinal Control of Elevator Hinge Moment
(1)
Verified
Elevator chord length for given hinge moment coefficient
Go
4 More Longitudinal Control of Elevator Hinge Moment 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 given Pull-down Maneuver Radius
Go
12 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 shear force, shear, friction and 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 given cutting force, cut size, uncut chip thickness, friction, rake and shear angles
Go
Created
Uncut chip thickness given cutting force, shear stress, cut, friction, normal rake and shear angles
Go
Created
Width of cut given cutting force, shear stress, uncut chip, friction, normal rake and shear angles
Go
14 More Merchant Force Circle (Mechanics of Orthogonal metal cutting) Calculators
Go
Normal Shock Waves
(12)
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 Normal Shock
Go
Created
Pressure Ratio across Normal Shock
Go
Created
Stagnation pressure behind normal shock by Rayleigh Pitot tube formula
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 Normal Shock
Go
8 More Normal Shock Waves Calculators
Go
Number of Connectors in Bridges
(5)
Verified
Effective Concrete Area given Force in Slab
Go
Verified
Force in Slab at Maximum Positive Moments given Minimum Number of Connectors for Bridges
Go
Verified
Force in Slab given Effective Concrete Area
Go
Verified
Minimum Number of Connectors for Bridges
Go
Verified
Steel Yield Strength given Total Area of Steel Section
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 Oblique Shock
Go
Created
Flow Deflection Angle using 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 Expansion Fan
Go
Created
Pressure Ratio across Oblique shock
Go
Created
Rearward Mach Angle of 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 Expansion Fan
Go
Created
Temperature Ratio across 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
Go
Verified
Efficiency of power transmission through nozzle for velocity and total head
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 using 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 using Pressure Coefficient
Go
Created
Total pressure in incompressible flow
Go
1 More Pressure Calculators
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
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 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
Stick Forces
(2)
Verified
Elevator Stick Force
Go
Verified
Elevator stick force for given hinge moment coefficient
Go
5 More Stick Forces 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 Circular Cylinder
Go
Created
Stream Function for non-lifting Flow over 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 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
Torque Required
(2)
Verified
Torque required considering power absorbed in journal bearing
Go
Verified
Torque required to overcome 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 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 given Lift Force and Weight of Aircraft
Go
Verified
Load Factor given Turn Radius
Go
Verified
Turn rate
Go
Verified
Velocity for given turn radius
Go
Verified
Velocity for given turn rate
Go
Verified
Weight for given load factor
Go
5 More Turning Flight Calculators
Go
Ultimate Shear Strength of Connectors in Bridges
(3)
Verified
Channel Web Thickness given Ultimate Shear Connector Strength for Channels
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 Airfoil
Go
5 More Velocity Calculators
Go
Velocity of Flow
(3)
Verified
Velocity of Flow at Outlet of Nozzle
Go
Verified
Velocity of Flow at outlet of Nozzle for Efficiency and Head
Go
Verified
Velocity of fluid in pipe for head loss at entrance of pipe
Go
6 More Velocity of Flow Calculators
Go
Velocity of Sound Wave
(1)
Verified
Velocity of Sound Wave considering Mach Angle in Compressible Fluid Flow
Go
5 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
4 More Viscosity of Fluid Calculators
Go
Viscous Flow
(1)
Verified
Total enthalpy in inviscid flow outside boundary layer
Go
14 More Viscous Flow Calculators
Go
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