Compressible Flow credits Logo credits
Potto Home Contact Us

Potto Home

About Potto

Chapters:

  Content
  Isentropic Flow
  Isothermal Nozzle
  Normal Shock
  Isothermal Flow
  Fanno Flow
  Rayleigh Flow
  Oblique Shock
  Prandtl-Meyer

Other things:
Download Area
calculators

Other Resources

  FAQs
  Compare Other Books
  Articles

Potto Statistics

License

Feedback

next up previous contents
Next: Isothermal Nozzle for k=1.67 Up: Isothermal Nozzle Previous: Isothermal Nozzle for k=1.3   Contents

Isothermal Nozzle for k=1.4

Isothermal Nozzle Flow Input: M k = 1.4
M T0/T0* P0/P0* A/A* P/P* PAR F/F*
1e-6 0.833333 1.06383 496585 2.01375 1e+6 416667
0.05 0.83375 1.06383 9.949 2.01023 19.9998 8.36242
0.1 0.835 1.06382 5.00074 1.99971 10 4.225
0.2 0.84 1.06371 2.55343 1.95815 5 2.2
0.25 0.84375 1.06354 2.07517 1.92755 4 1.8125
0.3 0.848333 1.06323 1.76292 1.8908 3.33333 1.56389
0.35 0.85375 1.06273 1.54585 1.84827 2.85714 1.39464
0.4 0.86 1.06196 1.38859 1.80038 2.5 1.275
0.45 0.867083 1.06086 1.27158 1.74761 2.22222 1.18843
0.5 0.875 1.05933 1.18311 1.69046 2 1.125
0.55 0.88375 1.0573 1.11582 1.62946 1.81818 1.07841
0.6 0.893333 1.05466 1.06484 1.56518 1.66667 1.04444
0.65 0.90375 1.05131 1.02689 1.49818 1.53846 1.02019
0.7 0.915 1.04717 0.999675 1.42904 1.42857 1.00357
0.75 0.927083 1.04212 0.981603 1.35832 1.33333 0.993056
0.8 0.94 1.03607 0.971556 1.2866 1.25 0.9875
0.85 0.95375 1.02892 0.968767 1.2144 1.17647 0.986029
0.9 0.968333 1.02058 0.972739 1.14225 1.11111 0.987963
0.95 0.98375 1.01097 0.983186 1.07063 1.05263 0.992763
1 1 1 1 1 1 1
1.05 1.01708 0.987614 1.02323 0.930764 0.952381 1.00933
1.1 1.035 0.973756 1.05305 0.863294 0.909091 1.02045
1.15 1.05375 0.958384 1.08979 0.797918 0.869565 1.03315
1.2 1.07333 0.941474 1.13392 0.734915 0.833333 1.04722
1.25 1.09375 0.923017 1.18602 0.674523 0.8 1.0625
1.3 1.115 0.903021 1.24687 0.61693 0.769231 1.07885
1.35 1.13708 0.881511 1.31738 0.562283 0.740741 1.09614
1.4 1.16 0.858533 1.39868 0.510686 0.714286 1.11429
1.45 1.18375 0.834148 1.4921 0.462204 0.689655 1.13319
1.5 1.20833 0.808437 1.59925 0.416862 0.666667 1.15278
1.55 1.23375 0.781495 1.72201 0.374655 0.645161 1.17298
1.6 1.26 0.753438 1.86264 0.335545 0.625 1.19375
1.65 1.28708 0.724391 2.0238 0.299467 0.606061 1.21503
1.7 1.315 0.694494 2.20863 0.266335 0.588235 1.23676
1.75 1.34375 0.663899 2.42089 0.236041 0.571429 1.25893
1.8 1.37333 0.632765 2.66502 0.208462 0.555556 1.28148
1.85 1.40375 0.601256 2.94634 0.183462 0.540541 1.30439
1.9 1.435 0.569542 3.27116 0.160896 0.526316 1.32763
1.95 1.46708 0.537792 3.64706 0.140612 0.512821 1.35118
2 1.5 0.506175 4.08308 0.122456 0.5 1.375
2.25 1.67708 0.355563 7.63559 0.058207 0.444444 1.49769
2.5 1.875 0.228809 15.7795 0.0253494 0.4 1.625
2.75 2.09375 0.134337 35.9507 0.0101149 0.363636 1.75568
3 2.33333 0.0717579 90.1421 0.00369786 0.333333 1.88889
3.25 2.59375 0.0348089 248.414 0.00123863 0.307692 2.02404
3.5 2.875 0.0153166 751.625 0.000380129 0.285714 2.16071
3.75 3.17708 0.0061097 2494.88 0.000106886 0.266667 2.29861
4 3.5 0.00220875 9078.88 2.75364e-5 0.25 2.4375
4.25 3.84375 0.000723666 36200.6 6.49973e-6 0.235294 2.57721
4.5 4.20833 0.000214915 158090 1.40567e-6 0.222222 2.71759
4.75 4.59375 5.787e-5 755855 2.78527e-7 0 2.85855
5 5 1.41334e-5 3.95528e+6 5.05653e-8 0 3
5.25 5.42708 3.13199e-6 2.26466e+7 8.41079e-9 0 3.14187
5.5 5.875 6.30011e-7 1.41846e+8 1.2818e-9 0 3.28409
5.75 6.34375 1.15084e-7 9.71693e+8 1.78979e-10 0 3.42663
6 6.83333 1.90985e-8 7.27886e+9 2.28973e-11 0 3.56944
6.25 7.34375 2.88057e-9 5.96147e+10 2.6839e-12 0 3.7125
6.5 7.875 3.95024e-10 5.33752e+11 2.88235e-13 0 3.85577
6.75 8.42708 4.92716e-11 5.2236e+12 2.83613e-14 0 3.99923
7 9 5.59183e-12 5.58723e+13 2.55685e-15 0 4.14286
7.25 9.59375 5.77621e-13 6.53098e+14 2.11195e-16 0 4.28664
7.5 10.2083 5.43254e-14 8.34215e+15 1.59831e-17 0 4.43056
7.75 10.8437 4.65335e-15 1.16429e+17 1.10825e-18 0 4.5746
8 11.5 3.63125e-16 1.7754e+18 7.04066e-20 0 4.71875
8.25 12.1771 2.5822e-17 2.95772e+19 4.09816e-21 0 4.86301
8.5 12.875 1.6737e-18 5.38293e+20 2.18556e-22 0 5.00735
8.75 13.5937 9.89062e-20 1.07018e+22 1.06791e-23 0 5.15179
9 14.3333 5.32996e-21 2.32407e+23 4.78089e-25 0 5.2963
9.25 15.0937 2.61982e-22 5.51286e+24 1.96102e-26 0 5.44088
9.5 15.875 1.17476e-23 1.42832e+26 7.36974e-28 0 5.58553
9.75 16.6771 4.80666e-25 4.04178e+27 2.5376e-29 0 5.73024
10 17.5 1.79484e-26 1.24913e+29 8.00557e-31 0 5.875
20 67.5 1.27091e-115 9.94074e+119 5.02981e-122 0 11.6875
30 150.833 2.10486e-266 6.67415e+271 4.99439e-274 0 17.5139
40 267.5 0 inf 0 0 23.3438
50 417.5 0 inf 0 0 29.175


Created by:Genick Bar-Meir, Ph.D.
On: 2007-12-04


These tables were generated using Potto-GDC (gas dynamics calculator) and also available in pdf version.



About Potto Project

Potto Project has been created by Dr. Genick Bar-Meir and friends to build free software, educational material and textbooks for college students.

Potto Project is under open content licenses, which means that you will always have the freedom to use it, make copies of it, and improve it. You are encouraged to make use of these freedoms and share the textbooks and program with your family and friends!

Copyright (C) 2007, 2006, 2005, 2004, 2003 Dr. Genick Bar-Meir.
Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or later or Potto license.
Site feedback please mail to barmeir at gmail.com