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 84
... load factor n . Later , we will discuss the range of permissible load factors in greater detail . We can now write the bank angle & in terms of the load factor $ = a cos 1 n [ 4.60 ] Let us now derive an expression for the turning ...
... load factor n . Later , we will discuss the range of permissible load factors in greater detail . We can now write the bank angle & in terms of the load factor $ = a cos 1 n [ 4.60 ] Let us now derive an expression for the turning ...
Page 85
... load factor and the velocity of the aircraft 8 V n2 -- 1 1 w = [ 4.66 ] The F - 16 Turning Radius For high - performance military aircraft , it is not the structure but the pilot who is the limiting factor for the maximum load factor . The ...
... load factor and the velocity of the aircraft 8 V n2 -- 1 1 w = [ 4.66 ] The F - 16 Turning Radius For high - performance military aircraft , it is not the structure but the pilot who is the limiting factor for the maximum load factor . The ...
Page 88
Dava J. Newman. Rearranging Equation ( 4.73 ) to produce the load factor in terms of the radius yields 2 n = 1 - rg [ 4.74 ] Since the radius , the velocity squared , and g are all positive quantities , the load factor n must be negative ...
Dava J. Newman. Rearranging Equation ( 4.73 ) to produce the load factor in terms of the radius yields 2 n = 1 - rg [ 4.74 ] Since the radius , the velocity squared , and g are all positive quantities , the load factor n must be negative ...
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