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 77
... Range of an Aircraft In this section we derive equations that will allow us to calculate the range and endurance of an aircraft . The range is defined as the total distance an aircraft can traverse on a tank of fuel . Related to range ...
... Range of an Aircraft In this section we derive equations that will allow us to calculate the range and endurance of an aircraft . The range is defined as the total distance an aircraft can traverse on a tank of fuel . Related to range ...
Страница 81
... range . Performing the forward integration , we obtain the following expression for the range of a jet aircraft : R = 2 2g C2 μ V POS CD · ( √mo + m , - - √mo ) [ 4.50 ] We see that the maximum range for a jet - powered aircraft is ...
... range . Performing the forward integration , we obtain the following expression for the range of a jet aircraft : R = 2 2g C2 μ V POS CD · ( √mo + m , - - √mo ) [ 4.50 ] We see that the maximum range for a jet - powered aircraft is ...
Страница 234
... range . For comparison purposes , the first two rocket types are for large - thrust rockets , whereas the others are ... range from 0.1 to 50 N , while large orbit control thrusters can range from 100 to 2,500 N. Table 10.4 | Various ...
... range . For comparison purposes , the first two rocket types are for large - thrust rockets , whereas the others are ... range from 0.1 to 50 N , while large orbit control thrusters can range from 100 to 2,500 N. Table 10.4 | Various ...
Съдържание
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
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