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Write an Algorithm and C-program to find the molar volume and specific volume of a mixture using Vandewaal's equation.
Solve the following system of equations using Gauss-siedel methods
Write a C-program to find the cubic polynomial equation to represent the relation between temperature and thermal conductivity. Use the following Data : Solve by Forward interpolation method
Write the step by step procedure to explain the Lagrange's method of interpolation and Newton's divided difference formula.
Write an algorithm and C-program to find time necessary to achieve given conversion in a Batch reactor using Simpson's 1/3rd Rule.
valuated by using
D) Trapezoidal rule ii) Simpson's 1/3 rule iii) Simpson's 3/8 rule
Compare the results with its actual value.
The ordinary differential equation write a C program to generate x y. Data for range insteps of 0.2. Use IV order Runge Kutta method.
The mass fraction of a sieve sample is related by a mathematical expression with initial condition, y=1 at x =0. Find the value of y for x = 0.1 by using Euler's method. Also write an Algorithm for the same.
Write a C-program and Algorithm to calculate the pressure drop, friction factor for the given velocities and to obtain a selection between f and Nro
Write a note on Arrhenius equation.
Write an Algorithm to evaluate the Dew point for a multi component ideal mixture.
Write a C-program to evaluate the vapor and liquid flow rates and composition for a multi component system in a flash drum.
Write the steps involved in the calculation of Area, Number of hair pins and pressure drop for a double pipe heat exchanger.
Write a C-program to calculate Adiabatic flame temperature for the given problem below. A Gas furnace burns propane Fuel. A balanced chemical reaction for complete combustion is
Assume pure propane is used, complete combustion takes place and Air-fuel ratio is 28. Specific heat capacity C, varies with temperature, Cpi = ai + bi T+ CiT2. Both propane and air enter at temperate 'T'.
Write a C-program to calculate the Area, number of tubes and pressure drop in a shell and Tube Heat Exchanger.
Write an Algorithm to determine the volume of Adiabatic CSTR.
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by using
write a C program to generate x y. Data for range 
insteps of 0.2. Use IV order Runge Kutta method. 
with initial condition, y=1 at x =0. Find the value of y for x = 0.1 by using Euler's method. Also write an Algorithm for the same. 