The performance of a jet, rocket, nuclear, ion or electric propulsion system can always be analyzed by four fundamental parameters, i.e., pressure, temperature, density and velocity inside the system. However, instead of using three physical properties of gases , three thermodynamic properties of gases are often used for convenience of calculations. Therefore, analysis of propulsion problems can be made by the application of the fundamentals of thermodynamics and aerothermodynamics. In this chapter, these fundamentals of thermodynamics and aerothermodynamics which are particularly applicable to propulsion problems will be given briefly but adequately. Extensive treatment or discussion of these subjects should, of course, be referred to the separate textbooks of thermodynamics and aerothermodynamics.
Research Article: Hydrology: Current Research
Research Article: Hydrology: Current Research
Research Article: Hydrology: Current Research
Research Article: Hydrology: Current Research
Research Article: Hydrology: Current Research
Research Article: Hydrology: Current Research
Research Article: Hydrology: Current Research
Research Article: Hydrology: Current Research
Research Article: Hydrology: Current Research
Research Article: Hydrology: Current Research
Accepted Abstracts: Environmental & Analytical Toxicology
Accepted Abstracts: Environmental & Analytical Toxicology
Posters & Accepted Abstracts: Environmental & Analytical Toxicology
Posters & Accepted Abstracts: Environmental & Analytical Toxicology
Scientific Tracks Abstracts: Environmental & Analytical Toxicology
Scientific Tracks Abstracts: Environmental & Analytical Toxicology
Posters: Hydrology: Current Research
Posters: Hydrology: Current Research
Scientific Tracks Abstracts: Hydrology: Current Research
Scientific Tracks Abstracts: Hydrology: Current Research
Hydrology: Current Research received 2843 citations as per Google Scholar report
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