Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 pages 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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Page 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 ...
Page 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 ...
Page 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 ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
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Expressions et termes fréquents
aerodynamic aerospace aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere balloon body calculated CD-ROM chapter coefficient components compressor crew member Decavitator defined density design process drag drawing ellipse energy Equation example Figure flight force fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift lines low Earth orbit LTA vehicle lunar magnetic field magnetosphere maneuver materials maximum microgravity mission module motion multiview NASA nozzle object onboard operational orbital mechanics oxygen parameters particles payload percent performance plane planetary pressure problem propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight spacesuit design specific speed stability structural subsystem surface temperature thermal thrust turbine units Van Allen belts vector vehicle design velocity wing