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 79
... tion , we see that if we want to achieve the maximum possible range , we need to fly at the maximum lift - to - drag ratio . Now let us find the endurance for a propeller - driven aircraft . Using Equa- tion ( 4.32 ) and recalling ...
... tion , we see that if we want to achieve the maximum possible range , we need to fly at the maximum lift - to - drag ratio . Now let us find the endurance for a propeller - driven aircraft . Using Equa- tion ( 4.32 ) and recalling ...
Страница 170
... tion 8.3.3 , " Low Earth Orbit , " define the important details of the microgravity environment . 8.3.2 Law of Gravitation Two of the most colorful personalities in the field of astronautics were Johannes Kepler and Sir Isaac Newton ...
... tion 8.3.3 , " Low Earth Orbit , " define the important details of the microgravity environment . 8.3.2 Law of Gravitation Two of the most colorful personalities in the field of astronautics were Johannes Kepler and Sir Isaac Newton ...
Страница 179
... tion are discussed below , namely , galactic cosmic rays and the Van Allen belts . Section 8.5 , " The Magnetosphere , " follows the discussion of ionizing radiation and details the Earth's magnetic field and implications for space ...
... tion are discussed below , namely , galactic cosmic rays and the Van Allen belts . Section 8.5 , " The Magnetosphere , " follows the discussion of ionizing radiation and details the Earth's magnetic field and implications for space ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
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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