SAE AIR1168/1-1990
Thermodynamics of Incompressible and Compressible Fluid Flow

Standard No.
SAE AIR1168/1-1990
Release Date
1990
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AIR1168/1-1990(R2004)
Latest
SAE AIR1168/1A-2019
Scope
The 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. 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 (Kt and 4fL/D), compressible flow analysis should be used.

SAE AIR1168/1-1990 history

  • 2019 SAE AIR1168/1A-2019 Thermodynamics of Incompressible and Compressible Fluid Flow
  • 2011 SAE AIR1168/1-2011 Thermodynamics of Incompressible and Compressible Fluid Flow
  • 0000 SAE AIR1168/1-1990(R2004)
  • 1990 SAE AIR1168/1-1990 Thermodynamics of Incompressible and Compressible Fluid Flow
  • 1989 SAE AIR1168/1-1989 Thermodynamics of Incompressible and Compressible Fluid Flow

SAE AIR1168/1-1990 -All Parts

SAE AIR1168/1-2011 Thermodynamics of Incompressible and Compressible Fluid Flow SAE AIR1168/10-2011 THERMOPHYSICAL CHARACTERISTICS OF WORKING FLUIDS AND HEAT TRANSFER FLUIDS SAE AIR1168/10A-2017 Thermophysical Characteristics of Working Fluids and Heat Transfer Fluids SAE AIR1168/11-2008 Spacecraft Boost and Entry Heat Transfer SAE AIR1168/11A-2011 Spacecraft Boost and Entry Heat Transfer SAE AIR1168/12-2004 Spacecraft Thermal Balance SAE AIR1168/12A-2011 Spacecraft Thermal Balance SAE AIR1168/13-2006 Spacecraft Equipment Environmental Control SAE AIR1168/13A-2011 Spacecraft Equipment Environmental Control SAE AIR1168/14-2011 Spacecraft Life Support Systems SAE AIR1168/14A-2012 Spacecraft Life Support Systems SAE AIR1168/1A-2019 Thermodynamics of Incompressible and Compressible Fluid Flow SAE AIR1168/2-2007 Heat and Mass Transfer and Air-Water Mixtures SAE AIR1168/2A-2011 Heat and Mass Transfer and Air-Water Mixtures SAE AIR1168/3-2011 Aerothermodynamic Systems Engineering and Design SAE AIR1168/3A-2019 SAE Aerospace Applied Thermodynamics Manual Aerothermodynamic Systems Engineering and Design SAE AIR1168/4-2004 Ice, Rain, Fog, and Frost Protection SAE AIR1168/4A-2014 SAE Aerospace Applied Thermodynamics Manual Ice, Rain, Fog, and Frost Protection SAE AIR1168/4B-2016 SAE Aerospace Applied Thermodynamics Manual Ice@ Rain@ Fog@ and Frost Protection SAE AIR1168/4C-2021 SAE Aerospace Applied Thermodynamics Manual Ice, Rain, Fog, and Frost Protection SAE AIR1168/5-2006 Aerothermodynamic Test Instrumentation and Measurement SAE AIR1168/5A-2011 Aerothermodynamic Test Instrumentation and Measurement SAE AIR1168/6-2004 Characteristics of Equipment Components, Equipment Cooling System Design, and Temperature Control System Design SAE AIR1168/6A-2011 Characteristics of Equipment Components@ Equipment Cooling System Design@ and Temperature Control System Design SAE AIR1168/7-2004 Aerospace Pressurization System Design SAE AIR1168/7A-2011 Aerospace Pressurization System Design SAE AIR1168/8-2004 Aircraft Fuel Weight Penalty Due to Air Conditioning SAE AIR1168/8A-2011 Aircraft Fuel Weight Penalty Due to Air Conditioning SAE AIR1168/9-2004 Thermophysical Properties of the Natural Environment, Gases, Liquids, and Solids SAE AIR1168/9A-2011 Thermophysical Properties of the Natural Environment, Gases, Liquids, and Solids



Copyright ©2024 All Rights Reserved