DYNAMICS OF AIRCRAFT FLIGHT
Performance calculations can be classified into three main types: lift, thrust and slope. Firstly, since the lift profile is known and unmodifiable from the time an aircraft is designed, the mass at a given speed or the speed at a given mass must be determined. Then, once the thrust of the engines a...
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| Main Author | |
|---|---|
| Format | Electronic eBook |
| Language | English |
| Published |
[S.l.] :
JOHN WILEY,
2022.
|
| Subjects | |
| Online Access | Full text |
| ISBN | 9781119988267 1119988268 1786307197 9781786307194 |
| Physical Description | 1 online resource |
Glossary of Terms