Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 страници This text contains an integrated bound-in CD-ROM, and has a strong emphasis on design. Its active visual approach and inclusion of space-orientated engineering make it an interesting examination of the aerospace engineering field. |
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Страница 44
... pressure term on both sides of the equation is called static pressure , and the previously defined dynamic pressure is added to the static pressure . The static pressure plus the dynamic pressure equals the total pressure . Fluid ...
... pressure term on both sides of the equation is called static pressure , and the previously defined dynamic pressure is added to the static pressure . The static pressure plus the dynamic pressure equals the total pressure . Fluid ...
Страница 125
... pressure by a factor of 4. In the cen- trifugal compressor , the additional pressure increase results from turning the flow radially . A similar single - stage axial compressor increases the pressure by only a factor of 1.2 , but ...
... pressure by a factor of 4. In the cen- trifugal compressor , the additional pressure increase results from turning the flow radially . A similar single - stage axial compressor increases the pressure by only a factor of 1.2 , but ...
Страница 129
... pressure gradient helps keep the flow attached to the turbine blades , and the pressure drop across a single turbine stage can be much greater than the pressure increase across a corresponding compressor stage . A single turbine stage ...
... pressure gradient helps keep the flow attached to the turbine blades , and the pressure drop across a single turbine stage can be much greater than the pressure increase across a corresponding compressor stage . A single turbine stage ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Авторско право | |
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