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Rayleigh — Compressible Flow
0.01 to 0.1 · 1.40 dimensionless, 0.001 dimensionless, 2.40 dimensionless
Rayleigh flow — frictionless, constant-area duct flow with heating or cooling — tabulated property ratios as a function of Mach number. Calculated for specific heat ratio γ = 1.40 (air at standard conditions). Covers 150 Mach numbers from 0.010 to 50, with all relevant property ratios (T/T*, p/p*, ρ/ρ*, p₀/p₀*, A/A*, fL*/D, etc.) for design and analysis of compressible duct flow.
- 0.01Mach Number: 0.01mach number 0.01
- 0.02Mach Number: 0.02mach number 0.02
- 0.03Mach Number: 0.03mach number 0.03
- 0.04Mach Number: 0.04mach number 0.04
- 0.05Mach Number: 0.05mach number 0.05
- 0.06Mach Number: 0.06mach number 0.06
- 0.07Mach Number: 0.07mach number 0.07
- 0.08Mach Number: 0.08mach number 0.08
- 0.09Mach Number: 0.09mach number 0.09
- 0.1Mach Number: 0.1mach number 0.1