courses:201a:adm
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courses:201a:adm [2018/02/20 18:16] evan |
courses:201a:adm [2018/04/16 21:35] (current) evan |
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| ===== Effect of Weight and C.G. on Aircraft Performance/Flight Char. ===== | ===== Effect of Weight and C.G. on Aircraft Performance/Flight Char. ===== | ||
| + | |||
| + | * Overloaded aircraft | ||
| + | * The aircraft needs a higher takeoff speed, which results in a longer takeoff run. | ||
| + | * Both the rate and angle of climb are reduced. | ||
| + | * The service ceiling is lowered. | ||
| + | * The cruising speed is reduced. | ||
| + | * The cruising range is shortened. | ||
| + | * Maneuverability is decreased. | ||
| + | * A longer landing roll is required because the landing speed is higher. | ||
| + | * Excessive loads are imposed on the structure, especially the landing gear. | ||
| + | |||
| + | Aft CG | ||
| + | * Higher cruise speed | ||
| + | * Less stability in pitch | ||
| + | * Difficult to recover from stall | ||
| + | * Shorter takeoff roll | ||
| + | |||
| + | Forward CG | ||
| + | * Longer takeoff roll | ||
| + | * Longer landing roll | ||
| + | * Slower cruise speed | ||
| + | * Difficult or impossible to land on main gear (insufficient elevator authority) | ||
| ==== Overloaded Aircraft ==== | ==== Overloaded Aircraft ==== | ||
courses/201a/adm.1519150594.txt.gz · Last modified: 2018/02/20 18:16 by evan
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