Values tabulated include -- pressure ratio, temperature ratio, area ratio, nondimensional mass flow with respect to total pressure, nondimensional mass flow with respect to static pressure, and velocity divided by square root of total temperature; applicability of tables to various propulsion calculations.
Compressible gas flow tables for specific heat ratio γ=4/3 (mach number 0.000 to 2.000)
Canada. Nat Research Council -- Aeronautical Report
1962
40 pages
Report
English
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