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AIR1168_1A

contributor authorSAE - SAE International
date accessioned2019-08-04T07:51:34Z
date available2019-08-04T07:51:34Z
date copyright4/11/2019 12:00:00 AM
date issued2019
identifier otherAIR1168_1A.pdf
identifier urihttp://yse.yabesh.ir/std;jsessioutho1603177793325273135A68A10958014A0/handle/yse/273923
description abstractThe fluid flow treated in this section is isothermal, subsonic, and incompressible. The effects of heat addition, work on the fluid, variation in sonic velocity, and changes in elevation are neglected. An incompressible fluid is one in which a change in pressure causes no resulting change in fluid density. The assumption that liquids are incompressible introduces no appreciable error in calculations, but the assumption that a gas is incompressible introduces an error of a magnitude that is dependent on the fluid velocity and on the loss coefficient of the particular duct section or price of equipment. Fit 1A-1 shows the error in pressure drop resulting from assuming that air is incompressible.With reasonably small loss coefficients and the accuracy that is usually required in most calculations, compressible fluids may be treated as incompressible for velocities less than Mach 0.2. At higher velocities and for large loss coefficients (K(sub)t and 4fL/D), compressible flow analysis should be used.
languageEnglish
titleThermodynamics of Incompressible and Compressible Fluid Flowen
titleAIR1168_1Anum
typeStandard
treeSAE - SAE International:;2019
contenttypeFulltext
identifier DOI10.4271/AIR1168/1A


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