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# Calculators Created by Shikha Maurya Indian Institute of Technology (IIT), Bombay
108
Formulas Created
171
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 171 calculators across 68 different categories till date.
Verified Aerodynamic axial force
Verified Aerodynamic normal force
Verified Aerodynamic side force
Verified Angle of attack
Verified Pitching moment
Verified Pitching moment coefficient
Verified Side force coefficient
Verified Sideslip angle
9 More Aerodynamic Nomenclature Calculators
Verified Power required at sea-level condition
Verified Velocity at an altitude for given velocity at sea-level condition
Verified Velocity at sea-level condition
3 More Altitude Effects on Power Required and Available Calculators
Created Critical Density
Created Critical Pressure
Created Critical Temperature
3 More Basic Compressible Flow Calculators
Basics (1)
Created Isentropic compressibility for given density and speed of sound
6 More Basics Calculators
Verified Section Modulus of Steel Beam when Stress in Steel for Unshored Members is Given
9 More Bending Stresses Calculators
Verified Pressure coefficient combined with blast wave for the shuttle
Verified Pressure coefficient combined with blast wave for the shuttle at angle of attack
Verified Pressure coefficient for Blunt-nosed cylinder:
3 More Blast-wave part 2 Calculators
Verified Acceleration of bodies
Verified Mass of body B of smaller mass
Verified Tension in the string if both the bodies are freely hanging
Verified Acceleration of system with bodies one hanging free and other lying on rough horizontal plane
1 More Bodies connected by string, one hanging free, other lying on rough horizontal plane Calculators
Verified Acceleration in system
Verified Tension in string if only one body is freely suspended
Verified Coefficient of drag for Reynold number in the laminar boundary layer flow
Verified Drag force on the plate in boundary layer flow
Verified Reynold number for drag force on the plate in boundary layer flow
Verified Viscosity of liquid for drag force on the plate in boundary layer flow
Verified Width of the plate for drag force on the plate in boundary layer flow
16 More Boundary layer flow Calculators
Verified Adiabatic wall enthalpy using Stanton number
Verified Enthalpy of wall using Stanton number
Verified Nusselt number for hypersonic vehicle
Verified Reynolds number for given Nusselt's number, Stanton number and Prandtl number
Verified Skin friction coefficient for incompressible flow
15 More Boundary-Layer Equations for Hypersonic Flow: Self-Similar Solutions Calculators
Verified Circulation developed on the airfoil
3 More Circulation Calculators
Verified Lift coefficient for lift force in body moving on fluid
5 More Coefficient's Calculators
Verified Mach angle for the compressible fluid flow
Verified Velocity of fluid considering the Mach angle in the compressible fluid flow
11 More Compressible flow Calculators
Verified Moment produced by vertical tail for given side force
Verified Vertical tail angle of attack
Verified Vertical tail moment arm for given side force
Verified Vertical tail side force for given moment
11 More Contribution of Aircraft Components- Part 1 Calculators
Verified Moment produced by vertical tail for given moment coefficient
Verified Yawing moment coefficient when wingspan is given
12 More Contribution of Aircraft Components- Part 2 Calculators
Verified Vertical tail area for given vertical tail volume ratio
Verified Vertical tail moment arm for given vertical tail volume ratio
Verified Vertical tail volume ratio
Verified Wing area for given vertical tail volume ratio
Verified Wingspan for given vertical tail volume ratio
10 More Contribution of Aircraft Components- Part 3 Calculators
Created Cutting force for given force along shear force, shear,friction & normal rake angles
Created Cutting force for given resultant force in merchant circle, friction angle and normal rake angle
Created Cutting force for shear stress,width of cut,uncut chip thickness,friction,normal rake & shear angles
3 More Cutting Force Calculators
Verified Discharge over rectangle weir considering Bazin's formula
Verified Discharge over rectangle weir considering Francis's formula
Verified Discharge with velocity of approach
Verified Discharge without velocity of approach
9 More Discharge Calculators
Verified Coefficient of pitot-tube for velocity at any point
Verified Resultant force on bend for force along x and y-direction
4 More Dynamics of fluid flow Calculators
Verified Elevator chord length for given hinge moment coefficient
4 More Elevator Hinge Moment Calculators
Verified Total enthalpy in the inviscid flow outside the boundary layer
14 More Flat-Plate for Viscous flow case Calculators
Verified Lift Coefficient for given turn rate
Verified Load factor for given turn rate for a high-performance fighter aircraft
Verified Radius of turn for given lift coefficient
10 More Flight Envelope Calculators
Verified Area of the nozzle at outlet for maximum power transmission through nozzle
Verified Area of the pipe for maximum power transmission through nozzle
Verified Diameter of nozzle for maximum power transmission through nozzle
Verified Diameter of the equivalent pipe
Verified Discharge in the equivalent pipe
Verified Length of pipe for maximum power transmission through nozzle
Verified Length of the equivalent pipe
9 More Flow through pipes Calculators
Created Force along shear force for given R of merchant circle, shear, friction and normal rake angles
2 More Force Along The Shear Calculators
Verified Angle of attack for circulation developed on the airfoil
Verified Area of the body for lift force in a body moving on a fluid
Verified Chord length for circulation developed on the airfoil
Verified Lift force for a body moving in a fluid of certain density
Verified Pressure drag from total drag force on a sphere
Verified Skin friction drag from total drag force on a sphere
9 More Forces on sub-merged bodies Calculators
Created 2-D Lift coefficient for cylinder
Created Airspeed measurement by Pitot tube for low-speed incompressible flow
Created Airspeed measurement by venturi
Created Circulation by Kutta-Joukowski theorem
Created Freestream density by Kutta-Joukowski theorem
Created Freestream velocity by Kutta-Joukowski theorem
Created Height difference of manometric fluid for given pressure difference
Created Lift per unit span by Kutta-Joukowski theorem
Created Location of stagnation point outside cylinder for lifting flow
Created Radius of cylinder for non-lifting flow
Created Source Strength for 2-D incompressible source flow
Created Stagnation streamline equation for flow over semi-infinite body
Created Test section velocity for low speed wind tunnel in terms of height difference of manometric fluid
Created Test section velocity in low-speed wind tunnel
Created Velocity at a point on airfoil for given pressure coefficient and free-stream velocity
Verified Modified pressure equation for cylindrical blast wave
Verified Pressure ratio for blunt cylinder blast wave
Verified Pressure ratio for blunt slab blast wave
13 More Hypersonic Equivalence Principle and Blast-Wave Theory Calculators
Verified Blunt-nosed radial coordinate flat plate (first approximation):
8 More Hypersonic Flight Paths: Velocity-Altitude Map Calculators
Verified Density before shock formation for compression wave
Verified Local shock velocity equation
Verified Mach wave behind the shock
Verified Mach wave behind the shock with mach infinity
Verified New pressure after the shock formation, subtracted to velocity for expansion wave
Verified Pressure ratio for unsteady waves with subtracted induced mass motion for expansion waves
Verified Temperature ratio for unsteady compression waves
11 More Hypersonic Inviscid Flowfields: Exact Methods Calculators
Verified Distance of stagnation point S from source in flow past a half body
14 More Ideal flow or Potential flow Calculators
Created Boundary layer thickness for laminar flow
Created Boundary layer thickness for Turbulent flow
Created Center of pressure location for cambered airfoil
Created Lift coefficient for cambered airfoil
Created Lift coefficient for symmetrical airfoil by Thin airfoil theory
Created Moment coefficient about leading-edge for symmetrical airfoil by thin airfoil theory
Created Skin friction drag coefficient for flat plate in laminar flow
Created Skin friction drag coefficient for flat plate in Turbulent flow
Verified Stall velocity for given touchdown velocity
4 More Landing Performance Calculators
Verified Length of weir considering Bazin's formula without velocity approach
Verified Length of weir considering Francis's formula
Verified Length of weir or notch for velocity of approach
Verified Length of weir or notch without velocity of approach
4 More Length of Weir Calculators
Verified Loss of pressure head for viscous flow between two parallel plates
2 More Loss of Head Calculators
Verified Loss of head at the entrance of a pipe
Verified Loss of head in the equivalent pipe
6 More Loss of Head Calculators
Verified Velocity for a given pull-down maneuver radius
11 More Maneuvering Flight Calculators
Created Friction angle for given R of merchant circle, force along shear force,shear & normal rake angles
Created Normal rake angle for given Resultant force, force along shear force, shear & friction angles
Created R in merchant circle for given force along the shear force, shear, friction & normal rake angles
Created Resultant force in merchant circle for given cutting force, friction and normal rake angles
Created Shear angle for given Resultant force ,force along shear force,friction & normal rake angles
Created Shear stress for cutting force,width of cut,uncut chip thickness,friction,normal rake & shear angles
Created Uncut chip thickness for cutting force,shear stress,width of cut,friction,normal rake & shear angles
Created Width of cut for cutting force,shear stress,uncut chip thickness,friction,normal rake & shear angles
14 More Merchant Force Circle (Mechanics of Orthogonal metal cutting) Calculators
Created Critical speed of sound from Prandtl relation
Created Density ahead of normal shock using normal shock momentum equation
Created Density behind normal shock for given upstream density and Mach number
Created Density behind normal shock using normal shock momentum equation
Created Density ratio across a normal shock
Created Enthalpy ahead of normal shock from normal shock energy equation
Created Enthalpy behind of normal shock from normal shock energy equation
Created Pressure ratio across a normal shock
Created Stagnation pressure behind normal shock by Rayleigh Pitot tube formula
Created Static enthalpy behind normal shock for given upstream enthalpy and Mach number
Created Static enthalpy ratio across a normal shock
Created Static Pressure ahead of normal shock using normal shock momentum equation
Created Static pressure behind normal shock for given upstream pressure and Mach number
Created Static Pressure behind of normal shock using normal shock momentum equation
Created Static temperature behind normal shock for given upstream temperature and Mach number
Created Temperature ratio across a normal shock
Created Velocity ahead of normal shock by normal shock momentum equation
Created Velocity ahead of normal shock from normal shock energy equation
Created Velocity behind of normal shock by normal shock momentum equation
Created Velocity behind of normal shock from normal shock energy equation
Created Velocity upstream of shock using Prandtl relation
8 More Normal Shock Waves Calculators
Verified Effective Concrete Area when Force in Slab is Given
Verified Force in Slab at Maximum Positive Moments when Minimum Number of Connectors for Bridges is Given
Verified Force in Slab when Effective Concrete Area is Given
Verified Minimum Number of Connectors for Bridges
Verified Steel Yield Strength when Total Area of Steel Section is Given
13 More Number of Connectors in Bridges Calculators
Created Component of downstream Mach number normal to oblique shock for given normal upstream Mach number
Created Density behind oblique shock for given upstream density and normal upstream Mach number
Created Density ratio across the oblique shock
Created Flow deflection angle in terms of Prandtl Meyer function
Created Forward Mach angle of expansion fan
Created Prandtl Meyer function
Created Prandtl Meyer function at upstream Mach number
Created Pressure behind expansion fan
Created Pressure behind oblique shock for given upstream pressure and normal upstream Mach number
Created Pressure ratio across the expansion fan
Created Pressure ratio across the oblique shock
Created Rearward Mach angle of the expansion fan
Created Temperature behind expansion fan
Created Temperature behind oblique shock for given upstream temperature and normal upstream Mach number
Created Temperature ratio across the expansion fan
Created Temperature ratio across the oblique shock
3 More Oblique Shock and Expansion Waves Calculators
Verified Power absorbed in overcoming viscous resistance in journal bearing
2 More Power Absorbed Calculators
Verified Efficiency of power transmission through nozzle for velocity and total head
Verified Efficiency of power transmission through the nozzle
1 More Power Transmission Efficiency Calculators
Created Dynamic pressure in incompressible flow
Created Pressure at a downstream point on streamline by Bernoulli's equation
Created Pressure at an upstream point on streamline by Bernoulli's equation
Created Pressure Coefficient
Created Pressure coefficient in terms of velocity ratio for incompressible flow
Created Pressure difference in low-speed wind tunnel for given test section velocity
Created Pressure difference measured by manometer in low-speed wind tunnel
Created Static pressure in incompressible flow
Created Surface pressure coefficient for lifting flow over circular cylinder
Created Surface pressure coefficient for non-lifting flow over circular cylinder
Created Surface pressure on body in terms of Pressure coefficient
Created Total pressure in incompressible flow
Created Radial velocity for 2-D incompressible source flow
Created Radial velocity for lifting flow over circular cylinder
Created Radial velocity for non-lifting flow over circular cylinder
Verified Excess power
Verified Total Drag for given excess power
8 More Rate of Climb Calculators
Verified Overall skin-friction drag coefficient
14 More Reference Temperature Method Calculators
Verified Elevator deflection angle for given stick force
Verified Elevator Stick Force
Verified Elevator stick force for given hinge moment coefficient
Verified Gearing ratio for given stick force
Verified Stick deflection angle for given gearing ratio
13 More Relationship between Stick Force and Hinge Moment Calculators
Verified Rotational speed considering power absorbed and torque in journal bearing
2 More Rotational Speed Calculators
Verified Horizontal Shear Range at the juncture of Slab and Beam
11 More Shear Range Calculators
Verified Enthalpy equation using coefficient of pressure for calorically perfect gas
Verified Free stream enthalpy
Verified Total enthalpy
8 More Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations Calculators
Created Stream function for 2-D Doublet flow
Created Stream function for 2-D incompressible source flow
Created Stream function for 2-D Vortex flow
Created Stream function for flow over Rankine oval
Created Stream function for lifting flow over a circular cylinder
Created Stream function for non-lifting flow over a circular cylinder
Created Stream function for semi-infinite body
Created Stream function for uniform incompressible flow
Created Stream function for uniform incompressible flow in polar coordinates
Verified Angle of attack at the tail
Verified Downwash angle
Verified Pitching moment due to tail
Verified Tail Pitching moment for given moment coefficient
Verified Total Lift Coefficient of wing-tail combination
16 More Tail Contribution Calculators
Verified Horizontal tail area for given tail volume ratio
Verified Horizontal tail volume ratio
Verified Tail moment arm for given horizontal tail volume ratio
Verified Wing Mean aerodynamic chord for given horizontal tail volume ratio
Verified Wing Reference area for given horizontal tail volume ratio
9 More Tail Contribution Contd Calculators
Verified Coefficient of rolling friction during ground roll
Verified Drag during ground effect
Verified Ground effect factor
Verified Lift acting on aircraft during ground roll
Verified Liftoff distance
Verified Maximum Lift coefficient for given liftoff velocity
Verified Resistance force during ground roll
Verified Stall velocity for given weight
Verified Thrust for given liftoff distance
Verified Weight of aircraft during ground roll
4 More Takeoff Performance Calculators
Created Tangential velocity for 2-D Vortex flow
Created Tangential velocity for lifting flow over circular cylinder
Created Tangential velocity for non-lifting flow over circular cylinder
Verified Absolute altitude
Verified Geometric altitude
Verified Geometric altitude for given geopotential altitude
Verified Geopotential altitude
Verified Lapse rate
Verified Torque required considering power absorbed in journal bearing
Verified Torque required to overcome the shear force in journal bearing
3 More Torque Required Calculators
Verified Average height of irregularities for turbulent flow in pipes
Verified Power required to maintain the turbulent flow
Verified Roughness Reynold number for turbulent flow in pipes
4 More Turbulent flow Calculators
Verified Bank angle during level turn
Verified Load factor given Lift Force and Weight
Verified Turn rate
Verified Velocity for a given turn radius
Verified Velocity for a given turn rate
Verified Weight for a given load factor
5 More Turning Flight Calculators
Verified Channel Web Thickness when Ultimate Shear Connector Strength for Channels is Given
Verified Elastic Modulus of Concrete when Ultimate Shear Connector Strength for Welded Studs is Given
Verified Ultimate Shear Strength for Welded Studs
6 More Ultimate Shear Strength of Connectors in Bridges Calculators
Verified Velocity of airfoil for circulation developed on the airfoil
5 More Velocity Calculators
Verified Velocity of flow at the outlet of the nozzle
Verified Velocity of flow at the outlet of the nozzle for efficiency and head
Verified Velocity of fluid in pipe for head loss at the entrance of a pipe
6 More Velocity of Flow Calculators
Verified Velocity of sound wave considering Mach angle in the compressible fluid flow
4 More Velocity of Sound Wave Calculators
Created Velocity potential for 2-D doublet flow
Created Velocity potential for 2-D source flow
Created Velocity potential for 2-D Vortex flow
Created Velocity potential for uniform incompressible flow
Created Velocity potential for uniform incompressible flow in polar coordinates
Verified Viscosity of fluid or oil for capillary tube method
3 More Viscosity of Fluid Calculators
Verified Diameter of capillary tube
Verified Difference of pressure for viscous flow between two parallel plates
Verified Discharge in capillary tube method
Verified Length for difference of pressure in viscous flow between two parallel plates
Verified Length for pressure head loss in viscous flow between two parallel plates
Verified Length of tube in capillary tube method
Verified Shear force for torque and diameter of shaft in journal bearing
Verified Shear stress in the fluid or oil of journal bearing
12 More Viscous flow Calculators
Verified Non dimensional internal energy parameter using wall-to-freestream temperature ratio
Verified Non dimensional static enthalpy
Verified Stanton equation using Overall skin friction coefficient for incompressible flow
13 More Viscous Flow: Basic Aspects, Boundary Layer Results, and Aerodynamic Heating Calculators Let Others Know