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Aircraft Propulsion, 2nd Edition by Saeed Farokhi

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APPENDIX DRayleigh Flow

The parameters corresponding to a Rayleigh line, for a calorically perfect gas (i.e., γ = constant), are summarized below:

(D.1)numbered Display Equation
(D.2)numbered Display Equation
(D.3)numbered Display Equation
(D.4)numbered Display Equation
(D.5)numbered Display Equation
(D.6)numbered Display Equation

We have derived these expressions in Chapter 2.

Rayleigh Flow γ = 1.4

M p/p* T/T * ρ/ρ* Tt/T  pt/p s/R
0.10 2.3669E+00 5.6020E−02 4.2250E+01 4.6777E−02 1.2591E+00 1.0949E+01
0.12 2.3526E+00 7.9698E−02 2.9519E+01 6.6606E−02 1.2554E+00 9.7088E+00
0.14 2.3359E+00 1.0695E−01 2.1842E+01 8.9471E−02 1.2510E+00 8.6724E+00
0.16 2.3170E+00 1.3743E−01 1.6859E+01 1.1511E−01 1.2461E+00 7.7865E+00
0.18 ...

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