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 127
... specific heat coefficient is a known property of air . We solve Equation ( 6.16 ) for the value of the fuel - to - air ratio , which allows us to precisely determine the engine's specific fuel consumption . As explained in Chapter 4 ...
... specific heat coefficient is a known property of air . We solve Equation ( 6.16 ) for the value of the fuel - to - air ratio , which allows us to precisely determine the engine's specific fuel consumption . As explained in Chapter 4 ...
Page 146
... specific thrust ? What is the thrust specific fuel consumption ? ( b ) What does increasing the compressor efficiency achieve ? ( c ) An increase in Mach number has what effect on thrust specific fuel consumption and specific thrust ...
... specific thrust ? What is the thrust specific fuel consumption ? ( b ) What does increasing the compressor efficiency achieve ? ( c ) An increase in Mach number has what effect on thrust specific fuel consumption and specific thrust ...
Page 324
... Specific heat capacity at constant pressure Cp 1,003.5 J / ( kg K ) • Specific heat capacity at constant volume Cv 716.5 J / ( kg⚫K ) Ratio of specific heat capacities 1.4006 Specific gas constant R 287 J / ( kg⚫K ) Speed of sound a ...
... Specific heat capacity at constant pressure Cp 1,003.5 J / ( kg K ) • Specific heat capacity at constant volume Cv 716.5 J / ( kg⚫K ) Ratio of specific heat capacities 1.4006 Specific gas constant R 287 J / ( kg⚫K ) Speed of sound a ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
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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