- 注册时间
- 2010-3-22
- 最后登录
- 2011-1-10
- 在线时间
- 1 小时
- 阅读权限
- 10
- 积分
- 0
- 帖子
- 5
- 精华
- 0
- UID
- 2661
![Rank: 1](static/image/common/star_level1.gif)
|
Flight profiles, engine thrusts and aeroplane flight speeds might be supplied
7 z$ k* R# h3 f. f: P& R; _directly for an aeroplane type undergoing reference flight procedures (see 4.2.2). Then, for
8 z& y. o4 X+ I" \6 d1 z8 soperations at an airport where the actual procedures in use are unknown, these reference! i; r" ]& x% I3 r6 {
procedures can be assumed. The information for other procedures known to be used, or for" g. w/ r+ J& Q" A$ A
different operating conditions of the aeroplane, can be calculated using aerodynamic and thrust
7 J/ F! y0 F5 L# ~4 wequations. |
|