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NASA-RP-1181
Simplified curve fits for the thermodynamic properties of equilibrium ai
Year: 1987
Abstract: New, improved curve fits for the thermodynamic properties of equilibrium air have been developed. The curve fits are for pressure, speed of sound, temperature, entropy, enthalpy, density, and internal energy. These curve fits can be readily incorporated into new or existing computational fluid dynamics codes if real gas effects are desired. The curve fits are constructed from Grabau-type transition functions to model the thermodynamic surfaces in a piecewise manner. The accuracies and continuity of these curve fits are substantially improved over those of previous curve fits. These improvements are due to the incorporation of a small number of additional terms in the approximating polynomials and careful choices of the transition functions. The ranges of validity of the new curve fits are temperatures up to 25 000 K and densities from 10 to the -7 to 10 to the 3d power amagats.
Subject: AIR
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:59:53Z | |
| date available | 2017-09-04T17:59:53Z | |
| date copyright | 01/01/1987 | |
| date issued | 1987 | |
| identifier other | FVHOEEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/182959 | |
| description abstract | New, improved curve fits for the thermodynamic properties of equilibrium air have been developed. The curve fits are for pressure, speed of sound, temperature, entropy, enthalpy, density, and internal energy. These curve fits can be readily incorporated into new or existing computational fluid dynamics codes if real gas effects are desired. The curve fits are constructed from Grabau-type transition functions to model the thermodynamic surfaces in a piecewise manner. The accuracies and continuity of these curve fits are substantially improved over those of previous curve fits. These improvements are due to the incorporation of a small number of additional terms in the approximating polynomials and careful choices of the transition functions. The ranges of validity of the new curve fits are temperatures up to 25 000 K and densities from 10 to the -7 to 10 to the 3d power amagats. | |
| language | English | |
| title | NASA-RP-1181 | num |
| title | Simplified curve fits for the thermodynamic properties of equilibrium ai | en |
| type | standard | |
| page | 54 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1987 | |
| contenttype | fulltext | |
| subject keywords | AIR | |
| subject keywords | APPROXIMATION | |
| subject keywords | COMPUTATIONAL FLUID DYNAMICS | |
| subject keywords | CURVE FITTING | |
| subject keywords | ENTHALPY | |
| subject keywords | ENTROPY | |
| subject keywords | EQUILIBRIUM FLOW | |
| subject keywords | HYPERSONIC FLOW | |
| subject keywords | POLYNOMIALS | |
| subject keywords | PRESSURE | |
| subject keywords | TEMPERATURE | |
| subject keywords | THERMODYNAMIC PROPERTIES |