Viscous heat dissipation
 

I am M. Sc. Engineering student. I am working on project, " Study of viscous heat dissipation effects at the tip of a cone(10 deg half angle) using Fluent Code." So far i have found velocity and temperature distributions for 0 deg angle of attack using Fluent code for compressible flow(air) at Mach Nos. of 1, 1.5, 1.8, 2, 3, 4, 5. For the verification of my results i need data related to my project. I have a plan to find the velocity and temperature distribution for 5 and 10 deg angle of attacks for the same Mach nos. I will be very thankful for any helpful guidance. My postal address is Muhammad Asif, C--115, CNS Hostels, P. O. Nilore, Islamabad, Pakistan.