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362  Chapter 11  The Equations of Change for Nonisothermal Systems

                     11A.3.  Transpiration cooling.
                           (a)  Calculate the temperature distribution between the two shells  of Example  11.4-4 for  radial
                           mass flow rates  of zero and 10"°  g/s  for  the following  conditions:

                                                    R = 500 microns  T R  = 300°C
                                                   KR  = 100 microns  T  = 100°C
                                                                       K
                                                    к = 6.13 X 10~ cal/cm  -s  -C
                                                                5
                                                   C p  = 0.25 cal/g  • С
                            (b)  Compare the rates  of  heat conduction to the surface  at KR in the presence and absence  of
                           convection.
                     11A.4.  Free-convection heat loss from  a vertical  surface.  A  small heating panel consists  essentially
                           of  a flat, vertical,  rectangular  surface  30  cm high  and  50  cm wide.  Estimate the total rate  of
                           heat  loss  from  one side  of  this panel by  free  convection, if  the panel surface  is  at  150°F, and
                           the surrounding air is at 70°F and 1 atm. Use the value  С = 0.548 of Lorenz in Eq. 11.4-51 and
                           the value  of С recommended by Whitaker, and compare the results  of the two calculations.
                           Answer: 8.1 cal/sec by Lorenz expression

                     11A.5.  Velocity,  temperature, and pressure  changes in a shock wave.  Air  at 1 atm and  70°F is flow-
                           ing at an upstream Mach number of 2 across a stationary shock wave. Calculate the  following
                           quantities, assuming  that у is constant at  1.4 and that C p  = 0.24 Btu/lb  m  •  F:
                            (a)  The initial velocity  of the air.
                            (b)  The velocity, temperature, and pressure downstream from the shock wave.
                            (c)  The changes  of internal and kinetic energy  across the shock wave.
                           Answer:  (a) 2250  ft/s
                                   (b) 844 ft/s;  888  R; 4.48 atm
                                   (c) AU  = +61.4 Btu/lb ; AK -  86.9 Btu/lb
                                                     w              m
                     11A.6.  Adiabatic  frictionless  compression  of  an  ideal  gas.  Calculate  the  temperature attained  by
                            compressing  air, initially  at  100°F and  1 atm, to 0.1  of  its initial volume. It is assumed  that у =
                            1.40  and that the compression  is  frictionless  and adiabatic. Discuss  the result  in relation to the
                            operation of an internal combustion engine.
                           Answer: 950°F

                     11 A.7.  Effect  of  free convection on  the insulating value of  a horizontal air space.  Two large  parallel
                            horizontal metal plates are separated by a 2.5 cm air gap, with the air at an average temperature
                            of  100°C. How much hotter may  the lower  plate be (than the upper plate) without causing the
                            onset of the cellular free convection discussed  in Example 11.5-2? How much may this tempera-
                            ture difference  be increased  if a very thin metal sheet is placed midway  between the two plates?
                           Answers: Approximately  3 and 48°C,  respectively.
                     11B.1.  Adiabatic frictionless processes in  an ideal  gas.
                            (a)  Note that a gas  that obeys  the ideal gas  law  may deviate  appreciably  from  C p  = constant.
                            Hence, rework  Example  11.4-6 using  a molar heat capacity expression  of the form



                            (b)  Determine the final pressure, p , required  if methane (CH ) is to be heated from  300K and
                                                       2
                                                                             4
                            1  atm to  800K by  adiabatic frictionless  compression. The recommended empirical constants  1

                               1
                                 O. A. Hougen, K. M. Watson, and R. A. Ragatz, Chemical Process Principles, Part 1,2nd edition, Wiley,
                            New York (1958), p. 255. See also Part II, pp. 646-653, for a fuller  discussion  of isentropic process calculations.
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