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Gas Tables for compressible flow calculations by S M Yahya Book Details
| Book Name | Gas Tables for compressible flow calculations |
| Author | S M Yahya |
| Category | Mechanical Engineering Books, Education Books |
| Book Language | English |
| Publisher | New Age International Publishers |
| Pages | 159 |
| ISBN | 8122423221 |
| Country | India |
| Book Size | 845 KB |
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About Gas Tables for compressible flow calculations by S M Yahya Book
Gas tables for compressible flow calculations are reference resources that provide valuable data and information about the thermodynamic properties of gases, particularly under conditions of high velocity and significant changes in pressure. These tables are commonly used by engineers and researchers in fields such as aerospace engineering, gas dynamics, propulsion systems, and fluid mechanics to analyze and design systems involving compressible flows.
Compressible flows occur when the density changes significantly due to variations in pressure and temperature. Examples include the flow of gases in jet engines, rocket nozzles, and supersonic aircraft.
Key information provided in gas tables for compressible flow calculations includes:
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Mach Number: The Mach number is a dimensionless parameter that indicates the speed of an object (usually an aircraft or fluid flow) relative to the speed of sound in the surrounding medium. It's an essential parameter in compressible flow calculations.
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Stagnation Properties: Stagnation conditions refer to the state of the fluid when it comes to rest. Stagnation properties include stagnation temperature, stagnation pressure, stagnation density, and stagnation enthalpy.
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Ratio of Specific Heats (γ): This parameter, also known as the adiabatic index or heat capacity ratio, characterizes the heat transfer characteristics of a gas. It's the ratio of the specific heat at constant pressure (Cp) to the specific heat at constant volume (Cv).
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Isentropic Relations: These relations describe the behavior of a fluid undergoing a reversible, adiabatic (no heat transfer) process. Isentropic relations are essential for understanding compressible flows.
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Prandtl-Meyer Function: This function helps calculate the turning angle of a supersonic flow over a curved surface, such as an airfoil.
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Critical Conditions: The critical conditions of a gas occur when the speed of sound equals the fluid velocity. Beyond this point, the flow is considered choked, and no further increase in flow rate is possible.
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Density Ratio: The ratio of the local density of the gas to its density at a reference state.
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Pressure Ratio: The ratio of the local pressure of the gas to its pressure at a reference state.
These tables allow engineers to quickly retrieve essential information for various flow conditions without having to perform extensive calculations. They are particularly valuable in cases where the flow transitions from subsonic to supersonic or hypersonic speeds.
Gas tables for compressible flow calculations can be found in textbooks, handbooks, and reference materials focused on fluid dynamics, gas dynamics, and aerospace engineering. Additionally, software tools and online calculators may provide digital versions of gas tables for easier access and convenience in modern engineering practices.
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