7. The pressure and Mach number of Helium flowing through a channel at a certain location are found to be p = 30 psia, M

Business, Finance, Economics, Accounting, Operations Management, Computer Science, Electrical Engineering, Mechanical Engineering, Civil Engineering, Chemical Engineering, Algebra, Precalculus, Statistics and Probabilty, Advanced Math, Physics, Chemistry, Biology, Nursing, Psychology, Certifications, Tests, Prep, and more.
Post Reply
answerhappygod
Site Admin
Posts: 899603
Joined: Mon Aug 02, 2021 8:13 am

7. The pressure and Mach number of Helium flowing through a channel at a certain location are found to be p = 30 psia, M

Post by answerhappygod »

7 The Pressure And Mach Number Of Helium Flowing Through A Channel At A Certain Location Are Found To Be P 30 Psia M 1
7 The Pressure And Mach Number Of Helium Flowing Through A Channel At A Certain Location Are Found To Be P 30 Psia M 1 (332.94 KiB) Viewed 40 times
7. The pressure and Mach number of Helium flowing through a channel at a certain location are found to be p = 30 psia, Ma = 1.5. At a point further downstream the pressure is 15 psia. Assuming isentropic flow through the channel, determine the Mach number at the second point. Assume y=1.67 (see below for tables). Ans. Ma₂ = 1.98 One-Dimensional Isentropic Compressible-Flow Functions For an ideal gas with constant specific heat and molecular weight, Y 1.67 P A P M M Po Po 0 1.0000 1.75 1.312 0.1721 0.05 11.265 0.9979 1.80 1.351 0.1601 0.10 5.661 0.9917 1.85 1.392 0.1490 0.15 3.805 0.9815 1.90 1.436 0.1386 0.20 2.887 0.9674 1.95 1.482 0.1290 0.25 2.344 0.9497 2.00 1.530 0.1201 0.30 1.989 0.9286 2.05 1.580 0.1119 0.35 1.741 0.9046 2.10 1.632 0.1042 0.40 1.560 0.8780 2.15 1.687 0.09712 0.45 1.424 0.8491 2,20 1.744 0.09053 0.50 1.320 0.8184 2.25 1.803 0.08442 0.55 1.239 0.7862 2.30 1.865 0.07875 0.60 1.176 0.7529 2.35 1.929 0.07349 0.65 1.126 0.7190 2.40 1.995 0.06862 0.70 1.0874 0.6847 2.45 2.064 0.06410 0.75 1.0576 0.6503 2.50 2.135 0.05990 0.80 1.0351 0.6162 2.55 2,209 0.05601 0.85 1.0189 0.5826 2.60 2.285 0.05239 0.90 1.0080 0.5497 2.65 2.364 0.04903 0.95 1.0019 0.5177 2.70 2.445 0.04591 1.00 1.0000 0.4867 2.75 2.529 0.04301 1.05 1.0018 0.4568 2.80 2.616 0.04032 1.10 1.0071 0.4282 2.85 2.705 0.03781 1.15 1.0154 0.4009 2.90 2.797 0.03547 1.20 1.0266 0.3749 2.95 2.892 0.03330 1.25 1.0406 0.3502 3.0 2.990 0.03128 1.30 1.0573 0.3269 3.5 4.134 0.01720 1.35 1.0765 0.3049 4.0 5.608 0.009939 1.40 1.0981 0.2842 4.5 7.456 0.006007 1.45 1.122 0.2647 5.0 9.721 0.003778 1.50 0.2465 6.0 165(10)-$ 1.55 1.176 0.2295 7.0 807(10) 1.60 1.207 0.2136 8.0 429(10) 1.65 1.240 0.1988 9.0 244(10) 1.70 1.275 0.1850 10.0 147(10) 0 15.68 23.85 34.58 48.24 65.18
Join a community of subject matter experts. Register for FREE to view solutions, replies, and use search function. Request answer by replying!
Post Reply