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 42
... lift as a reaction to the airflow passing over it . Lift L signifies aerodynamic forces perpendicular to veloc- ity ... coefficient of lift and drag , respectively . [ See Equation ( 3.10 ) and Equation ( 3.11 ) . ] The lift ...
... lift as a reaction to the airflow passing over it . Lift L signifies aerodynamic forces perpendicular to veloc- ity ... coefficient of lift and drag , respectively . [ See Equation ( 3.10 ) and Equation ( 3.11 ) . ] The lift ...
Page 55
... coefficient of lift of the wing and AR is the aspect ratio of the wing . ( Note : This equation is only good for elliptical lift distribution in an incom- pressible flow , which produces uniform downwash distribution . Later we will ...
... coefficient of lift of the wing and AR is the aspect ratio of the wing . ( Note : This equation is only good for elliptical lift distribution in an incom- pressible flow , which produces uniform downwash distribution . Later we will ...
Page 56
... lift , and we write the coefficient of drag as CD . Finally , the total drag coefficient becomes CDTOTAL = CD2 + TEAR [ 3.34 ] Figure 3.5 gave the overall shape of coefficient of lift and coefficient of drag curves as a function of ...
... lift , and we write the coefficient of drag as CD . Finally , the total drag coefficient becomes CDTOTAL = CD2 + TEAR [ 3.34 ] Figure 3.5 gave the overall shape of coefficient of lift and coefficient of drag curves as a function of ...
Table des matières
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Droits d'auteur | |
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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