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Search: Posts Made By: Shendal
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Forum: Tech Log
27th Mar 2006, 16:04
Replies: 6
Views: 1,513
Posted By Shendal

Thanks all of you, I understand what I wanted to...

Thanks all of you, I understand what I wanted to know >:)
Forum: Tech Log
25th Mar 2006, 10:12
Replies: 6
Views: 1,513
Posted By Shendal

I mean, If the airplane fly at 300 Kt True...

I mean,

If the airplane fly at 300 Kt True Air Speed and there is 20 Kt of headwind, it means it will be flying at 280 Kt ground speed.

On the other hand, it the same aircraft has a 20 kt of...
24th Mar 2006, 19:07
Replies: 13
Views: 1,085
Posted By Shendal

Use this one: ...

Use this one:
http://www.worldstart.com/weekly-download/archives/reg-cleaner4.3.htm
24th Mar 2006, 19:02
Replies: 212
Views: 27,129
Posted By Shendal

I have a logiteck 3D force feedback and it works...

I have a logiteck 3D force feedback and it works fine :)
It is not very expensive, I paid for it about 40 pounds one year ago.
Forum: Tech Log
24th Mar 2006, 17:25
Replies: 6
Views: 1,513
Posted By Shendal

Question How wind affects required thrust ?

I would like to know how wind affects required thrust and fuel flow on the cruise phase.
Forum: Tech Log
24th Mar 2006, 13:55
Replies: 9
Views: 1,393
Posted By Shendal

Is not the maximal value for the C.I., 200 ? ...

Is not the maximal value for the C.I., 200 ?

I just realize that where I write sqrt(CL)/CD it may say CL/CD.
Forum: Tech Log
24th Mar 2006, 12:44
Replies: 9
Views: 1,393
Posted By Shendal

Acronyms

Here are all acronyms I have used:

C.I. = Cost Index
V_x = Speed for best angle of climb
V_y = Speed for best rate of climb
CL = Lift coefficient
CD = Drag coefficient
SFC = Specific Fuel...
Forum: Tech Log
24th Mar 2006, 09:05
Replies: 9
Views: 1,393
Posted By Shendal

Smile Some questions about Performance

Hello,

My questions are:

If a climb is done in the thrust position of Max Climb, and with C.I.=0 the airplane may climb at V_x and with a C.I. = 200 it may climb at V_y. Then if we apply the...
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