Calculators Created by Sai Venkata Phanindra Chary Arendra

Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
https://www.linkedin.com/in/arendra-sai-venkata-phanindra-chary-1a5b76139
122
Formulas Created
261
Formulas Verified
73
Across Categories

List of Calculators by Sai Venkata Phanindra Chary Arendra

Following is a combined list of all the calculators that have been created and verified by Sai Venkata Phanindra Chary Arendra. Sai Venkata Phanindra Chary Arendra has created 122 and verified 261 calculators across 73 different categories till date.
Created Absorbed radiation in terms of absorptivity and incident radiation
Go
Created Absorbed radiation in terms of incident, reflected and transmitted radiation
Go
Created Absorptivity
Go
Created Absorptivity in terms of reflectivity and transmissivity
Go
Created Absorptivity in terms of reflectivity for opaque surface
Go
Created Incident radiation in terms of absorbed, reflected and transmitted radiation
Go
Created Incident radiation in terms of absorptivity and absorbed energy
Go
Created Incident radiation in terms of reflectivity and reflected radiation
Go
Created Incident radiation in terms of transmissivity and transmitted radiation
Go
Created Reflected radiation in terms of incident, absorbed and transmitted radiation
Go
Created Reflected radiation in terms of reflectivity and incident radiation
Go
Created Reflectivity in terms of absorptivity and transmissivity
Go
Created Reflectivity in terms of absorptivity for opaque surface
Go
Created Reflectivity in terms of reflected radiation and incident radiation
Go
Created Transmissivity in terms of absorptivity and reflectivity
Go
Created Transmissivity in terms of transmitted radiation and incident radiation
Go
Created Transmitted radiation in terms of incident, absorbed and reflected radiation
Go
Created Transmitted radiation in terms of transmissivity and incident radiation
Go
Verified Diameter of the measuring wires
Go
Verified Micrometer measurement/reading
Go
Verified Pitch diameter
Go
Verified Pitch of screw
Go
Verified Free stream enthalpy over a flat plate with freestream conditions
Go
Verified Free stream velocity over a flat plate using drag force
Go
Verified Free stream velocity over a flat plate with freestream conditions
Go
Verified Freestream density over the flat under the freestream flow conditions
Go
Verified Insulated flat plate, the strong interaction
Go
Verified Total enthalpy over a flat plate with freestream conditions
Go
9 More Approximate Results Applied to Hypersonic Vehicles Calculators
Go
Created Diffuse solar radiation in terms of total solar energy and direct radiation
Go
Created Effective surface temperature of the sun in terms of solar constant
Go
Created Mean distance between sun/star and earth/planet
Go
Created Radius of the sun in terms of total solar irradiance
Go
Created Total solar energy incident on the unit area of a horizontal surface on the ground
Go
Created Total solar irradiance or solar constant
Go
Basics (4)
Created Thermal conductance for given thermal resistance
Go
Created Total thermal resistance for conduction through three resistances in series
Go
Created Total thermal resistance for conduction through two resistances in parallel
Go
Created Total thermal resistance for conduction through two resistances in series
Go
1 More Basics Calculators
Go
Basics (1)
Created Thermal resistance for conduction through 2 resistances in parallel
Go
6 More Basics Calculators
Go
Verified Diameter of the measuring wires
Go
Verified Micrometer measurement/reading
Go
Verified Pitch diameter
Go
Verified pitch of screw
Go
Verified Time period of oscillation in the ship
Go
Verified Volume of body in fluid for metacentric height and BG
Go
7 More Buoyancy Calculators
Go
Verified Charging current in relaxation circuit
Go
Verified Power supply during charging
Go
Verified Resistance of charging circuit
Go
Verified Time constant from charging current
Go
Verified Time elapsed during charging
Go
Verified Density of the fluid for stagnation considering compressible fluid flow
Go
Verified Mach number for the compressible fluid flow
Go
Verified Pressure at inlet considering maximum flow rate of fluid
Go
Verified Pressure at inlet of the tank or vessel considering compressible fluid flow
Go
Verified Stagnation density considering other stagnation properties of the fluid
Go
Verified Stagnation density considering the compressible fluid flow
Go
Verified Stagnation pressure considering other stagnation properties of the fluid
Go
Verified Stagnation pressure for the compressible fluid flow
Go
Verified Stagnation temperature considering other stagnation properties of the fluid
Go
Verified Velocity at the outlet of the nozzle for maximum flow rate of fluid
Go
Verified Velocity of sound wave in Mach number for the compressible fluid flow
Go
13 More Compressible flow Calculators
Go
Verified Freestream density
Go
Verified Freestream velocity
Go
2 More COMPUTATIONAL-FLUID-DYNAMIC SOLUTIONS Calculators
Go
Created Convection resistance for a cylindrical layer
Go
Created Heat flow rate through a cylindrical composite wall of 2 layers
Go
Created Heat flow rate through a cylindrical composite wall of 3 layers
Go
Created Heat flow rate through a cylindrical wall
Go
Created Inner surface temperature of a cylindrical wall for a given heat flow rate
Go
Created Length of the cylindrical wall for a given heat flow rate
Go
Created Outer surface temperature of a cylindrical wall for a given heat flow rate
Go
Created Outer surface temperature of the cylindrical composite wall of 2 layers
Go
Created Thermal conductivity of a cylindrical wall for a given temperature difference
Go
Created Thermal resistance for radial heat conduction offered by a cylinder wall
Go
Created Thickness of the cylindrical wall to maintain a given temperature difference
Go
Created Total thermal resistance of 2 cylindrical resistances connected in series.
Go
Created Total thermal resistance of 3 cylindrical resistances connected in series
Go
Created Total thermal resistance of a cylindrical wall with convection either side
Go
Created Emissive power in terms of radiation intensity for diffusely emitting surface
Go
Created Emissive power of diffusely emitted black body radiation in terms of radiation intensity
Go
Created Intensity of diffusely emitted radiation in terms of radiosity and reflected radiation
Go
Created Intensity of diffusely incident radiation in terms of irradiation
Go
Created Intensity of diffusely reflected radiation in terms of radiosity and emitted radiation
Go
Created Irradiation for a diffusely incident radiation
Go
Created Radiation intensity in terms of emissive power for diffusely emitting black body
Go
Created Radiation intensity in terms of emissive power for diffusely emitting surface
Go
Created Radiosity in terms of incident and reflected radiation
Go
Created Temperature of a diffusely emitting black body in terms of radiation intensity
Go
Created The intensity of radiation emitted by a black body at an absolute temperature
Go
Verified Coefficient of Drag for given thrust-to-weight ratio
Go
Verified Drag for a level, unaccelerated flight at negligible thrust angle
Go
Verified Zero-lift drag coefficient for given lift coefficient
Go
4 More Drag during Level Unaccelerated Flight Calculators
Go
Verified Mean free path using number density
Go
Verified Molar volume using kinetic energy per mole
Go
Verified Number density
Go
Verified Volume of gas
Go
11 More ELEMENTS OF KINETIC THEORY Calculators
Go
Verified Centrifugal Force in an accelerated flight
Go
Verified Drag for a level, unaccelerated flight
Go
Verified Drag in an accelerated flight
Go
Verified Lift for an unaccelerated flight
Go
Verified Lift in an accelerated flight
Go
Verified Thrust angle for an unaccelerated flight for given drag
Go
Verified Thrust angle for an unaccelerated flight for given lift
Go
Verified Thrust for a level, unaccelerated flight
Go
Verified Thrust in an accelerated flight
Go
Verified Velocity in an accelerated flight
Go
Verified Weight of aircraft in level, unaccelerated flight
Go
Verified Lift Coefficient for a given turn radius
Go
Verified Turn rate for a high load factor
Go
Verified Velocity for a given turn rate for a high load factor
Go
Verified Wing loading for a given turn rate
Go
11 More Flight Envelope Calculators
Go
Verified Area of flow for a circular channel
Go
Verified Chezy's constant considering Kutter's formula
Go
Verified Chezy's constant considering Manning's formula
Go
Verified Hydraulic mean depth considering Manning's formula
Go
Verified Manning's coefficient or constant
Go
Verified Radius of a circular channel considering wetted perimeter
Go
Verified Wetted perimeter for a circular channel
Go
12 More Flow in open channels Calculators
Go
Verified Atmospheric pressure
Go
Verified Dynamic viscosity of electrolyte
Go
Verified Flow rate of the electrolyte
Go
Verified Gap spacing
Go
Verified Pressure in flushing hole
Go
Verified Radius of flushing hole
Go
Verified Radius of the electrode
Go
Verified Loss of head due to sudden contraction
Go
Verified Velocity at section 2-2 for sudden contraction
Go
37 More Flow through pipes Calculators
Go
Verified Diameter of the wire used in three wire system method
Go
Verified Ideal wire diameter in three wire system method
Go
Verified Micrometer reading from three wire system method
Go
Verified Pitch diameter from three wire system method
Go
Verified Pitch of the thread from three wire system method
Go
Verified Pitch of thread when ideal wire diameter is known
Go
Verified Thread angle when ideal wire diameter is known
Go
Verified Angle of attack for lift coefficient on the airfoil
Go
Verified Circulation in the location of stagnation points
Go
Verified Coefficient of lift for an airfoil
Go
Verified Location of stagnation points for a rotating cylinder in a uniform flow field
Go
Verified Radius of the cylinder for location of stagnation points
Go
26 More Forces on sub-merged bodies Calculators
Go
Created Back rake angle for orthogonal cutting
Go
Created Cutting Speed
Go
Created Initial diameter of the job
Go
Created Machine Feed
Go
Created Number of jobs revolution per unit time
Go
Created Uncut chip thickness
Go
4 More Geometry of Turning Process Calculators
Go
Verified Drag for given glide angle
Go
Verified Glide angle
Go
3 More Gliding Flight Calculators
Go
Verified Blunt-nosed flat plate pressure ratio (first approximation)
Go
Verified formula For creation pressure for the planar blast wave
Go
Verified Modified Radial coordinate equation for cylindrical blast wave
Go
Verified Radial coordinate for the planar blast wave,
Go
Verified Radial coordinate of cylindrical blast wave
Go
11 More Hypersonic Equivalence Principle and Blast-Wave Theory Calculators
Go
Verified Radius of curvature for the cylinder-wedge
Go
Verified Radius of curvature for the sphere-cone body shape
Go
7 More Hypersonic Flight Paths: Velocity-Altitude Map Calculators
Go
Verified Non dimensional radius for hypersonic vehicles
Go
Verified Transformed conical variable
Go
Verified Transformed conical variable with wave angle
Go
9 More Hypersonic Inviscid Flowfields: Approximate Methods Calculators
Go
Verified Density before the shock formation for expansion wave
Go
Verified New pressure after the shock formation for compression wave
Go
Verified Ratio of new and old temperature for expansion waves
Go
Verified Temperature ratio for unsteady expansion wave
Go
14 More Hypersonic Inviscid Flowfields: Exact Methods Calculators
Go
Verified Doty and Rasmussen - normal-force coefficient
Go
Verified Rasmussen closed-form expression for the shock-wave angle
Go
15 More Hypersonic Small-Disturbance Equations Calculators
Go
Verified Mach number over a flat plate using static temperature and wall temperature
Go
Verified Static temperature of fluid over the flat plate
Go
Verified Static temperature of the plate using the wall viscosity
Go
Verified Static temperature over a flat plate under viscous, very high Mach flow
Go
Verified Total temperature over a flat plate under viscous Mach flow
Go
Verified Total temperature over a flat plate under viscous very high Mach flow
Go
Verified Wall temperature of fluid over the flat plate
Go
Verified Wall temperature of the plate using the wall viscosity
Go
10 More Hypersonic Viscous Interactions Calculators
Go
Verified Dimensions of Rankine half-body
Go
Verified Distance between source or sink from origin
Go
Verified Location of stagnation point on x-axis
Go
Verified Strength of source for Rankine half body
Go
Verified Uniform flow velocity for Rankine half body
Go
10 More Ideal flow or Potential flow Calculators
Go
Verified Angular velocity considering the depth of parabola
Go
Verified Depth of parabola formed at the free surface of water
Go
Verified Rate of flow or discharge
Go
Verified Resultant velocity for two velocity components
Go
3 More Kinematics of flow Calculators
Go
Created Absorptivity of a small body in terms of absorbed radiation and temperature
Go
Created Emissivity of a small body in terms of emitted radiation and temperature
Go
Created Radiation absorbed by the small body per unit of its surface area
Go
Created Radiation emitted by a small body
Go
Created Temperature of a small body in terms of absorptivity and absorbed radiation
Go
Created Temperature of a small body in terms of emissivity and emitted radiation
Go
Verified Touchdown velocity for given stall velocity
Go
4 More Landing Performance Calculators
Go
Verified Diameter of the measuring wires
Go
Verified Micrometer measurement/reading
Go
Verified Pitch diameter
Go
Verified pitch of screw
Go
Verified Load factor for a given pull-down maneuver rate
Go
Verified Load factor for a given pull-up maneuver radius
Go
Verified Pull-down maneuver rate
Go
Verified Pull-up maneuver radius
Go
8 More Maneuvering Flight Calculators
Go
Verified Area of cut from tool temperature
Go
Verified Cutting speed from tool temperature
Go
Verified specific cutting energy per unit cutting force from tool temperature
Go
Verified Specific heat of work from tool temperature
Go
Verified Thermal conductivity of work from tool temperature
Go
5 More Mechanics of orthogonal cutting Calculators
Go
Created Force normal to shear for given mean shear stress, width of cut, uncut chip thickness & shear angle
Go
Created Force normal to shear force for given mean normal shear stress & area of shear plane
Go
Created Mean normal stress in shear plane for given normal force & shear area
Go
35 More Merchant Force Circle (Mechanics of Orthogonal metal cutting) Calculators
Go
Created Lead (approach or entering) angle for given side cutting edge angle
Go
Created side cutting edge angle for given Lead (approach or entering) angle
Go
4 More Metal Cutting and tools Calculators
Go
Verified Tolerance unit (i)
Go
Verified Convective heat transfer to the surface
Go
1 More Modern design-oriented code Calculators
Go
Verified Steady state equimolal counter diffusion between gases (mass flux)
Go
Verified Steady state equimolal counter diffusion of component A into B ( mass flux)
Go
15 More Molar diffusion Calculators
Go
Verified Ambient atmospheric pressure
Go
Verified Net force acting on the electrode
Go
Verified Pressure in flushing hole
Go
Verified Coefficient of drag equation with angle of attack
Go
Verified Coefficient of lift equation with angle of attack
Go
Verified Drag force with angle of attack
Go
Verified Lift force with angle of attack
Go
Verified Pressure coefficient for slender bodies of revolution
Go
9 More Newtonian Flow Calculators
Go
Verified Characteristic Mach Number behind shock
Go
Verified Entropy change across normal shock
Go
Verified Relation between Characteristic Mach number and Mach number
Go
Verified Shock strength
Go
Verified Velocity behind a normal shock
Go
24 More Normal Shock Waves Calculators
Go
Verified Discharge over a broad-crested weir for head of liquid at middle
Go
Verified Discharge over a broad-crested weir with velocity approach
Go
Verified Discharge over a trapezoidal notch or weir
Go
Verified Discharge over a triangular notch or weir
Go
Verified Head of liquid above the V-notch
Go
Verified Length of weir for broad-crested weir and head of liquid at middle
Go
Verified Length of weir for broad-crested weir with velocity approach
Go
Verified Time required to empty a tank with a triangular weir or notch
Go
19 More Notches and Weirs Calculators
Go
Verified Component of Downstream Mach normal to oblique shock
Go
Verified Flow deflection angle
Go
17 More Oblique Shock and Expansion Waves Calculators
Go
Verified Absolute pressure head at constant head and atmospheric pressure head
Go
Verified Area of tank while considering time for emptying a tank
Go
Verified Atmospheric pressure head at constant head and absolute pressure head
Go
Verified Co-efficient of discharge
Go
Verified Co-efficient of discharge considering time for emptying a tank
Go
Verified Co-efficient of discharge for area and velocity
Go
Verified Co-efficient of velocity for horizontal and vertical distance
Go
Verified Loss of head due to sudden enlargement
Go
Verified Time of emptying a tank through an orifice at bottom
Go
Verified Velocity of liquid at C-C for Hc, Ha, and H
Go
23 More Orifices and Mouthpieces Calculators
Go
Created Heat flow rate through pipe with eccentric lagging
Go
Created Heat flow through pipe in square section
Go
Created inner surface temperature of a pipe in square section
Go
Created Inner surface temperature of a pipe with eccentric lagging
Go
Created Length of a pipe with eccentric lagging
Go
Created outer surface temperature of a pipe in square section
Go
Created outer surface temperature of a pipe with eccentric lagging
Go
Created Thermal conductivity for a pipe with eccentric lagging
Go
Created Thermal resistance for a pipe in square section
Go
Created Thermal resistance of a pipe with eccentric lagging
Go
Created Area of a composite wall of 2 layers
Go
Created Area of a composite wall of 3 layers
Go
Created Area of the plane wall required for a given temperature difference
Go
Created Heat flow rate through a composite wall of 2 layers in series
Go
Created Heat flow rate through a composite wall of 3 layers in series
Go
Created Inner surface temperature of a composite wall of 2 layers in series
Go
Created Inner surface temperature of a composite wall of 3 layers in series
Go
Created Inner surface temperature of a plane wall
Go
Created Interface temperature of composite wall of 2 layers when inner surface temperature is known
Go
Created Interface temperature of composite wall of 2 layers when outer surface temperature is known
Go
Created Length of the 2nd layer of the composite wall for a given temperature difference
Go
Created Length of the 3rd layer of the composite wall for a given temperature difference
Go
Created Outer surface temperature of a composite wall of 2 layers for a given heat flow rate
Go
Created Outer surface temperature of a composite wall of 3 layers for a given heat flow rate
Go
Created Outer surface temperature of the wall for a given heat flow rate
Go
Created Temperature at distance x from the inner surface in the wall
Go
Created Thermal conductivity of the material required to maintain a given temperature difference
Go
Created Thermal resistance of a composite wall with 2 layers in series
Go
Created Thermal resistance of a composite wall with 3 layers in series
Go
Created Thermal Resistance of a wall
Go
Created Thickness of the plane wall required for a given temperature difference
Go
Created Total thermal resistance of a plain wall with convection on either side
Go
Verified Elastic modulus of the composite in the transverse direction
Go
17 More Polymer Matrix Composites (PMC) Calculators
Go
Verified Overcut constant A
Go
Verified Overcut constant B
Go
Verified Overcut produced per side
Go
Verified Taper produced due to side sparks
Go
Verified Upper diameter of hole
Go
10 More Possible surface defects in EDM Calculators
Go
Verified Coefficient of Drag due to lift for minimum power required
Go
Verified Freestream velocity for given required power
Go
Verified Freestream Velocity for given total drag
Go
Verified Zero-lift drag coefficient for minimum power required
Go
6 More Power Required for Level Unaccelerated Flight Calculators
Go
Verified Atmospheric pressure at electrode tip
Go
Verified Pressure distribution in the flushing gap
Go
Verified Pressure in flushing hole
Go
Verified Radial location of pressure distribution
Go
Verified Radius of flushing hole
Go
Verified Radius of the electrode
Go
Created Radiation energy emitted by a black body in given time interval when emissive power is known
Go
Created Radiation energy emitted by a black body in given time interval when temperature is known
Go
Created Radiation energy emitted by a black body per unit time and surface area
Go
Created Spectral black body emissive power (Planck's law)
Go
Created Surface area of the black body required to emit certain amount of radiation energy
Go
Created Temperature of the black body to emit a certain amount of radiation energy
Go
Created Time required to emit a specified amount of radiation energy from the black body
Go
Verified Endurance of Jet Airplane
Go
Verified Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane
Go
5 More Range and Endurance of Jet Airplane Calculators
Go
Verified Excess power for given rate of climb
Go
Verified Velocity of aircraft at a given rate of climb
Go
Verified Velocity of aircraft for given excess power
Go
7 More Rate of Climb Calculators
Go
Verified Reynolds number for chord length
Go
Verified Static density of the plate using chord length for flat plate case
Go
Verified Static velocity of the plate using chord length for flat plate case
Go
13 More Reference Temperature Method Calculators
Go
Verified Diameter of the wire used
Go
Verified Micrometer measurement/reading
Go
Verified Pitch diameter
Go
Verified Pitch of screw threads
Go
Verified Enthalpy equation using specific heat ratio
Go
Verified local shock-layer thickness
Go
Verified total enthalpy equation using specific heat ratio and velocities
Go
8 More Space-Marching Finite Difference Method: Additional Solutions of the Euler Equations Calculators
Go
Spheres (11)
Created Convection resistance for a spherical layer
Go
Created Heat flow rate through a spherical composite wall of 2 layers in series
Go
Created Heat flow rate through a spherical wall
Go
Created Inner surface temperature of a spherical wall
Go
Created Outer surface temperature of a spherical wall
Go
Created Thermal resistance of a spherical composite wall of 2 layers in series with convection
Go
Created Thermal resistance of a spherical wall
Go
Created Thickness of the spherical wall to maintain given temperature difference
Go
Created Total thermal resistance of a spherical wall of 2 layers without convection
Go
Created Total thermal resistance of a spherical wall of 3 layers without convection
Go
Created Total thermal resistance of a spherical wall with convection on either side
Go
Verified Angle of attack of the wing
Go
20 More Tail Contribution Calculators
Go
Verified Maximum Lift coefficient for given stall velocity
Go
Verified Stall velocity for given liftoff velocity
Go
12 More Takeoff Performance Calculators
Go
Verified Coefficient of Drag due to lift
Go
Verified Drag Coefficient for given parasite drag coefficient
Go
Verified Drag Coefficient for given zero-lift drag coefficient
Go
1 More The Drag Polar Calculators
Go
Verified Diameter of the wire used in measurement over wires method
Go
Verified Micrometer reading from measurement over wires method
Go
Verified Pitch diameter from measurement over wires method
Go
Verified Pitch of the thread from measurement over wires method
Go
Verified Coefficient of Lift for given thrust-to-weight ratio
Go
Verified Lift for a level, unaccelerated flight at negligible thrust angle
Go
Verified Minimum Thrust required
Go
Verified Thrust required for level, unaccelerated flight
Go
Verified Weight of aircraft for a level, unaccelerated flight at negligible thrust angle
Go
7 More Thrust Required for Level Unaccelerated Flight Calculators
Go
Verified Tool temperature
Go
15 More Tool Life And Tool Wear Calculators
Go
Verified Lift during level turn
Go
Verified Lift for a given load factor
Go
Verified Load factor for a given turn rate
Go
Verified Turn radius
Go
8 More Turning Flight Calculators
Go
Verified Best size wire
Go
Verified Best wire size for modified buttress 45deg and 7deg
Go
Verified Micrometer reading/measurement
Go
Verified Pitch diameter
Go
Verified Pitch for modified buttress 45deg and 7deg
Go
Verified Pitch of screw
Go
Verified Diameter of shaft for speed and shear stress of fluid in journal bearing
Go
Verified Difference of pressure for viscous or laminar flow
Go
Verified External or outer radius of collar for total torque
Go
Verified Internal or inner radius of collar for total torque
Go
Verified Power absorbed in collar bearing
Go
Verified Power absorbed in foot-step bearing
Go
Verified Radius of shaft for torque required in foot-step bearing
Go
Verified Rotational speed for torque required in collar bearing
Go
Verified Rotational speed for torque required in foot-step bearing
Go
Verified Shear force or viscous resistance in journal bearing
Go
Verified Speed of rotation for shear force in journal bearing
Go
Verified Thickness of oil film for shear force in journal bearing
Go
Verified Thickness of oil film for speed and diameter of shaft in journal bearing
Go
Verified Thickness of oil film for torque required in foot-step bearing
Go
Verified Torque required to overcome viscous resistance in collar bearing
Go
Verified Torque required to overcome viscous resistance in foot-step bearing
Go
36 More Viscous flow Calculators
Go
Verified internal energy for hypersonic flow
Go
Verified Non dimensional internal energy parameter
Go
Verified Static enthalpy
Go
Verified Wall temperature calculator due to internal energy
Go
12 More Viscous Flow: Basic Aspects, Boundary Layer Results, and Aerodynamic Heating Calculators
Go
Verified Volume of electrode material worn out
Go
Verified Volume of work material removed
Go
Verified Wear Ratio
Go
Verified Diameter of the wire used
Go
Verified Micrometer reading/measurement
Go
Verified Pitch diameter
Go
Verified pitch of screw threads
Go
Share Image
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!