Computer Programs and Test Cases in Chapter 11

Convective Heat Transfer

Tuncer Cebeci

Computer Programs and Test Cases in Chapter 11

These computer programs correspond to those discussed in Chapter 11 and use the same designation as in that chapter. For example, the computer program for section 11.2 is named pr11_2.for for compressible boundary layer flows and, like the computer programs discussed in sections 11.3 to 11.9, includes a test case as discussed in subsection 11.2.7

A table of contents for the computer programs together with sample calculations are given below.

11.2 Fortran Program for Compressible Boundary-Layer Flows (pr11_2.for)
         PC executable file (pr11_2.exe)
                Test case:   a) input data:   upper part of NACA0012 airfoil (pr11_2Inp.txt)
                                  b) output (pr11_2Out.pdf)

11.3 Hess-Smith Panel Method (panel.for)
         PC executable file (panel.exe)
                Test case:   a) input data: NACA 0012 airfoil for 4 degree angle attack (n0012-183.txt)
                                  b) output (panelOut.txt)

11.4 Forced and Free Convection between Two Vertical Parallel Plates (pr11_4.for)
         PC executable file (pr11_4.exe)
                Test case:   a) input data
                                  b) output

11.5 Wall Jet and Film Heating (pr11_5.for)
         PC executable file (pr11_5.exe)
                Test case:   a) input data
                                  b) output

11.6 Turbulent Free Jet (pr11_6.for)
         PC executable file (pr11_6.exe)
                Test case:   a) input data
                                  b) output

11.7 Mixing Layer between Two Uniform Streams at Different Temperatures (pr11_7.for)
         PC executable file (pr11_7.exe)
                Test case:   a) input data
                                  b) output

11.8 Fortran Programs for Laminar and Turbulent Heat Transfer in a Pipe with Fully Developed Velocity Profile
                Test case 1:   a) computer program (pr11_8a.for)
                                     b) PC executable file (pr11_8a.exe)
                                     c) input data (pr11_8ainp.txt)
                                     d) output (pr11_8aout.pdf)
                Test case 2:   a) computer program (pr11_8b.for)
                                     b) PC executable file (pr11_8b.exe)
                                     c) input data (pr11_8binp.txt)
                                     d) output (pr11_8bout.pdf)
                Test case 2:   a) analytical (pr11_8ba.for)
                                     b) PC executable file (pr11_8ba.exe)
                                     c) input data (pr11_8bainp.txt)
                                     d) output (pr11_8baout.pdf)
                Test case 3:   a) computer program (pr11_8c.for)
                                     b) PC executable file (pr11_8c.exe)
                                              Case 1
                                              input data (pr11_8cinp1.txt)
                                                output (pr11_8cout1.pdf)

                                              Case 2
                                              input data (pr11_8cinp2.txt)
                                                output (pr11_8cout2.pdf)

                                              Case 3
                                              input data (pr11_8cinp3.txt)
                                                output (pr11_8cout3.pdf)

11.9 Fortran Programs for Calculating Momentum and Heat Transfer in Laminar and Turbulent Flows by Integral Methods
           Table 11.9 instructions for calculating momentum and heat transfer in laminar and turbulent flows
                Test case 1: Laminar and turbulent flow over an airfoil without heat transfer
                                    a) Follow 1, 2, 3, 5 and 6 instructions in Table 11.9
                                    b) Output summary
               Test case 2: Laminar and turbulent flow over an airfoil with heat transfer
                                    a) Follow all instructions in Table 11.9
                                    b) Output summary
                Test case 3: Laminar and turbulent flow over an uniformly heated ellipse
                                    a) Follow 3, 4, 5, 6, and 7 instructions in Table 11.9 with input file thwaitesIn3.txt
                                    b) Output summary

Table of Contents