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 56
... 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 airfoil angle of attack ...
... 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 airfoil angle of attack ...
Page 76
... coefficient reaches a maximum value . We saw that the maximum value of C is C , max , the lift coefficient at stalling . The slowest speed at which an aircraft can fly in a straight and level flight is therefore called the stalling ...
... coefficient reaches a maximum value . We saw that the maximum value of C is C , max , the lift coefficient at stalling . The slowest speed at which an aircraft can fly in a straight and level flight is therefore called the stalling ...
Page 336
... coefficient , moment , 152 , 153 coefficient , solar absorption , 167-69 coefficient , specific heat , 127 coefficient of drag , 42 , 48 , 52 total , 56 coefficient of lift defined , 42 , 48 equation , 75 and flight envelope , 89 and ...
... coefficient , moment , 152 , 153 coefficient , solar absorption , 167-69 coefficient , specific heat , 127 coefficient of drag , 42 , 48 , 52 total , 56 coefficient of lift defined , 42 , 48 equation , 75 and flight envelope , 89 and ...
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