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. |
À l'intérieur du livre
Résultats 1-3 sur 26
Page 125
... compressor increases the airflow 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 ...
... compressor increases the airflow 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 ...
Page 126
... compressor becomes a design constraint ( i.e. , a fac- tor limiting the engine performance ) due to temperature limits on the compres- sor material , especially the last compressor stage . 6.3.3 Burner or Combustor The burner is where ...
... compressor becomes a design constraint ( i.e. , a fac- tor limiting the engine performance ) due to temperature limits on the compres- sor material , especially the last compressor stage . 6.3.3 Burner or Combustor The burner is where ...
Page 129
... compressor stage . A single turbine stage can be used to drive multiple compressor stages . To keep flow from leak- ing around the edges of the turbine blades , because of the higher pressure gradi- ent , the tips of the turbine blades ...
... compressor stage . A single turbine stage can be used to drive multiple compressor stages . To keep flow from leak- ing around the edges of the turbine blades , because of the higher pressure gradi- ent , the tips of the turbine blades ...
Table des matières
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Droits d'auteur | |
15 autres sections non affichées
Autres éditions - Tout afficher
Expressions et termes fréquents
aerodynamic aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere axis balloon body Boeing burner calculate camber CD-ROM chapter coefficient coefficient of lift components compressor crew member debris Decavitator drag drawing efficiency elliptical energy Equation equilibrium example Figure flight force freestream fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift load factor low Earth orbit LTA vehicle lunar maneuver mass flow materials maximum microgravity mission motion NASA nozzle object operational orbital mechanics oxygen particles payload performance plane planetary pressure problem produced propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight specific speed stability static structural surface temperature thermal thrust truss turbine turbofan turbojet United vector velocity wing