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 9
... jet engine aircraft work is given in Chapter 6 , " Aircraft Propulsion . " Whittle had filed a patent in 1930 which became the basis for the British efforts to develop a jet engine , resulting in the first success- ful test of a turbojet ...
... jet engine aircraft work is given in Chapter 6 , " Aircraft Propulsion . " Whittle had filed a patent in 1930 which became the basis for the British efforts to develop a jet engine , resulting in the first success- ful test of a turbojet ...
Page 122
... turbine . Figure 6.3 shows a schematic of a jet engine with engine station numbers , which are useful in identifying the airflow through the various components . In Figure 6.3 | Jet , or gas turbine , engine schematic with station ...
... turbine . Figure 6.3 shows a schematic of a jet engine with engine station numbers , which are useful in identifying the airflow through the various components . In Figure 6.3 | Jet , or gas turbine , engine schematic with station ...
Page 132
... engines . 6.4 | FUNDAMENTAL EQUATIONS GOVERNING JET ENGINES We have described the gas turbine engine components and now want to solve for the thrust developed by the entire jet engine system . All the equations necessary to compute the ...
... engines . 6.4 | FUNDAMENTAL EQUATIONS GOVERNING JET ENGINES We have described the gas turbine engine components and now want to solve for the thrust developed by the entire jet engine system . All the equations necessary to compute the ...
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