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- W2151883387 abstract "A systematic method is presented for the specie cation of ramjet/scramjet test facility air simulant and fuel simulant composition and combustor or engine entrance conditions. An analysis of the governing equations is performed to identify a minimum set of dimensionless variables and dimensionless closure relationships. The enthalpy closure, which relates dimensionless enthalpy to dimensionless pressure, density, and composition, is studied. Best air simulant compositions for typical vitiated air facilities are identie ed by matching a simplie ed enthalpy closure relationship for the simulants to e ight. The air simulant compositions so identie ed are tested in simple calculations of a scramjet combustor and nozzle that assume two-stream, quasi-one-dimensional e ow and equilibrium chemistry. Results for the new simulation method arecompared with results for simulants constituted in the conventional manner and to e ight. Detailed effects of chemical kinetics, which are known to be important in many ramjet/scramjet simulations or in e ight, are not considered." @default.
- W2151883387 created "2016-06-24" @default.
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- W2151883387 date "1998-07-01" @default.
- W2151883387 modified "2023-09-24" @default.
- W2151883387 title "Specification of Model Entrance Conditions for Scramjet Testing in Vitiated Air" @default.
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- W2151883387 doi "https://doi.org/10.2514/2.500" @default.
- W2151883387 hasPublicationYear "1998" @default.
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