\"\"\" Breaking ice with air cushion \"\"\" import matplotlib.pyplot as plt import math import numpy as np #function f(x,y) def f(p,h): return(pow(p,3)*(1-pow(beta,2)))+(((0.4*h*pow(beta,2))-(sigma*pow(h,2)/pow(r,2)))*pow(p,2))+(((pow(sigma,2)*pow(h,4))/(3*pow(r,4)))*p)-(pow((sigma*pow(h,2)/(3*pow(r,2))),3)) #derivative…
abhishek007123 abhishek007123
updated on 10 Nov 2018
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Read more Projects by abhishek007123 abhishek007123 (3)
Breaking Ice with Air cushion Vehicle - Find minimum pressure with Newton-Raphson method
\"\"\" Breaking ice with air cushion \"\"\" import matplotlib.pyplot as plt import math import numpy as np #function f(x,y) def f(p,h): return(pow(p,3)*(1-pow(beta,2)))+(((0.4*h*pow(beta,2))-(sigma*pow(h,2)/pow(r,2)))*pow(p,2))+(((pow(sigma,2)*pow(h,4))/(3*pow(r,4)))*p)-(pow((sigma*pow(h,2)/(3*pow(r,2))),3)) #derivative…
10 Nov 2018 09:16 AM IST
Air standard Cycle USING PYTHON
import math import matplotlib.pyplot as plt def engine_kinematics(bore,stroke,con_rod,cr,start_crank,end_crank): \"\"\" Engine Kinematics \"\"\" #Geometric parameters a=stroke/2 R=con_rod/a #Volume Parameters V_s=math.pi*(1/4)*pow(bore,2)*stroke V_c=V_s/(cr-1) sc=math.radians(start_crank) ec=math.radians(end_crank) num_values=50…
06 Nov 2018 05:08 AM IST
Parsing NASA thermodynamic data using MATLAB
NOTE- ALL NECESSARY SCREENSHOTS AND PLOTS ARE UPLOADED TO GOOGLE DRIVE. The objective for this program is to write a function a function that extracts the 14 co-efficients and calculates the enthalpy, entropy and specific heats for all the species in the data file. NASA came up with polynomials that can…
10 Oct 2018 08:10 AM IST