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Search: Posts Made By: acad_l
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Forum: Rumours & News
21st Apr 2010, 18:30
Replies: 3,110
Views: 1,591,088
Posted By acad_l

One can simply divide by the by-pass ratio of...

One can simply divide by the by-pass ratio of 4.3.

But there is the issue, under which conditions is the mass flow rate 1177 lb/s? We probably should consider a density figure at pressure and...
Forum: Rumours & News
20th Apr 2010, 16:40
Replies: 3,110
Views: 1,591,088
Posted By acad_l

Right. I made an algebraic error. 32 g is it. ...

Right. I made an algebraic error. 32 g is it.

You can easily adapt to different times and conditions.
Forum: Rumours & News
20th Apr 2010, 16:11
Replies: 3,110
Views: 1,591,088
Posted By acad_l

Very wrong. You need to calculate the air flow...

Very wrong. You need to calculate the air flow through the engine. Nothing to do with thrust.

An example. Which I based upon figures from the Canadian VAAC, which seems to use a distinctly...
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