Consider a stoichiometric mixture of H2 and O2 at standard condition (298.15 K and 1.05 x 105 Pa,) at the upstream. The specific heat ratio of the mixture is 1.4. The heat of combustion for this stoichiometric mixture g. is 190.5 kJ/mole. The universal gas constant R =8. 314 J/mole/ K. (1) calculate the average molecular weight of the mixture MW, the local sound speed au, the density pu (2) if the upstream flow velocity u-1 m/s, plot the Rayleigh lines, and the Hugoniot hyperboles with its asymptotes. (3) if the upstream flow velocity u= 2000 m/s, what is the downstream detonation pressure po, and density Po
Consider a stoichiometric mixture of H2 and O2 at standard condition (298.15 K and 1.05 x 105 Pa,) at the upstream. The specific heat ratio of the mixture is 1.4. The heat of combustion for this stoichiometric mixture g. is 190.5 kJ/mole. The universal gas constant R =8. 314 J/mole/ K. (1) calculate the average molecular weight of the mixture MW, the local sound speed au, the density pu (2) if the upstream flow velocity u-1 m/s, plot the Rayleigh lines, and the Hugoniot hyperboles with its asymptotes. (3) if the upstream flow velocity u= 2000 m/s, what is the downstream detonation pressure po, and density Po
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![Consider a stoichiometric mixture of H2 and O2 at standard condition (298.15 K and 1.05 x 10$ Pa,) at the
upstream. The specific heat ratio of the mixture is 1.4. The heat of combustion for this stoichiometric
mixture q. is 190.5 kJ/mole. The universal gas constant R =8. 314 J/mole/ K.
(1) calculate the average molecular weight of the mixture MW, the local sound speed au, the density pu
(2) if the upstream flow velocity u- 1 m/s, plot the Rayleigh lines, and the Hugoniot hyperboles with
its asymptotes.
(3) if the upstream flow velocity y= 2000 m/s, what is the downstream detonation pressure pb, and
density po](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F334d14e9-a361-4a52-8014-0caf619ec15a%2Fb2974320-8fb4-4021-aabb-4b86bbcaa2ae%2Fx5jjecd_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Consider a stoichiometric mixture of H2 and O2 at standard condition (298.15 K and 1.05 x 10$ Pa,) at the
upstream. The specific heat ratio of the mixture is 1.4. The heat of combustion for this stoichiometric
mixture q. is 190.5 kJ/mole. The universal gas constant R =8. 314 J/mole/ K.
(1) calculate the average molecular weight of the mixture MW, the local sound speed au, the density pu
(2) if the upstream flow velocity u- 1 m/s, plot the Rayleigh lines, and the Hugoniot hyperboles with
its asymptotes.
(3) if the upstream flow velocity y= 2000 m/s, what is the downstream detonation pressure pb, and
density po
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