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 40
... wing geometry is initially introduced . Figure 3.1 shows a simple wing geometry , similar to that found on a light gen- eral aviation aircraft , as viewed from above ( top view ) . The front of the wing , at the left , is called the ...
... wing geometry is initially introduced . Figure 3.1 shows a simple wing geometry , similar to that found on a light gen- eral aviation aircraft , as viewed from above ( top view ) . The front of the wing , at the left , is called the ...
Page 41
... wing surface area and is written as AR = b2 S The aspect ratio is a measure of how long and slender a wing is from tip to tip . For a rectangular wing this reduces to the ratio of the span to the chord length . High - aspect - ratio wings ...
... wing surface area and is written as AR = b2 S The aspect ratio is a measure of how long and slender a wing is from tip to tip . For a rectangular wing this reduces to the ratio of the span to the chord length . High - aspect - ratio wings ...
Page 154
... wing by itself is unbalanced . To correct the situation , a horizontal stabi- lizer is mounted behind the wing . If the wing is inclined downward to produce a negative lift , then a clockwise moment about the cg will be created . If ...
... wing by itself is unbalanced . To correct the situation , a horizontal stabi- lizer is mounted behind the wing . If the wing is inclined downward to produce a negative lift , then a clockwise moment about the cg will be created . If ...
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