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 55
... elliptical lift distribution in an incom- pressible flow , which produces uniform downwash distribution . Later we will show how we can still use this substitution to arrive at the formula for induced drag using an efficiency factor ...
... elliptical lift distribution in an incom- pressible flow , which produces uniform downwash distribution . Later we will show how we can still use this substitution to arrive at the formula for induced drag using an efficiency factor ...
Page 204
... elliptical orbit of a body can be characterized by its semi- major axis and its eccentricity . The semimajor axis a of an ellipse can be described as one - half the length of the longitudinal axis of the ellipse . The eccen- tricity e ...
... elliptical orbit of a body can be characterized by its semi- major axis and its eccentricity . The semimajor axis a of an ellipse can be described as one - half the length of the longitudinal axis of the ellipse . The eccen- tricity e ...
Page 205
... elliptical orbit . [ 9.12 ] b Ул X C F A a e a The eccentric anomaly can be constructed by circumscribing a circle around the elliptical orbit of the body ; this circle is tangent to the two ends of the ellipse ( at perigee and apogee ...
... elliptical orbit . [ 9.12 ] b Ул X C F A a e a The eccentric anomaly can be constructed by circumscribing a circle around the elliptical orbit of the body ; this circle is tangent to the two ends of the ellipse ( at perigee and apogee ...
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