Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 страници 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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Страница 84
... 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 Φ = a cos 1 n [ 4.60 ] Let us now derive an expression for the turning radius of ...
... 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 Φ = a cos 1 n [ 4.60 ] Let us now derive an expression for the turning radius of ...
Страница 85
... factor and the velocity of the aircraft 8V n2 - 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 ...
... factor and the velocity of the aircraft 8V n2 - 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 ...
Страница 88
... factor , Equation ( 4.59 ) , and substitute Equa- tion ( 4.19 ) in for lift : L pv2C1S n = = W W [ 4.76 ] Expressing n in terms of the wing loading , we have the following equation that relates flight velocity v to load factor : = nmax ...
... factor , Equation ( 4.59 ) , and substitute Equa- tion ( 4.19 ) in for lift : L pv2C1S n = = W W [ 4.76 ] Expressing n in terms of the wing loading , we have the following equation that relates flight velocity v to load factor : = nmax ...
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A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
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