Re: [Flightgear-devel] f16 speedbrakes

2008-09-07 Thread Jon S. Berndt
This would be good to see in a plot. Can you do that?

Jon


 -Original Message-
 From: [EMAIL PROTECTED]
 [mailto:[EMAIL PROTECTED] On Behalf Of
 Alex Romosan
 Sent: Saturday, September 06, 2008 5:06 PM
 To: FlightGear developers discussions
 Subject: Re: [Flightgear-devel] f16 speedbrakes
 
 Jon S. Berndt writes:
 
  I don't know if this matters, but remember that not too long ago we
  added the ability to enter aero coefficients in several coordinate
  systems - including BODY and WIND, etc.
 
 so if i were to represent the wind tunnel data in x,y,z axis then the
 drag due to horizontal tail deflection (the data on pages 45-49 of the
 nasa technical paper 1538) would then look like this:
 
 axis name=X
   function name=aero/coefficient/CDDh
 descriptionDrag_due_to_horizontal_tail_deflection/description
 product
   propertyaero/qbar-psf/property
   propertymetrics/Sw-sqft/property
   table name=CDdHT


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Re: [Flightgear-devel] f16 speedbrakes

2008-09-07 Thread Alex Romosan
Jon S. Berndt writes:

 This would be good to see in a plot. Can you do that?

i guess jsbsim can do it but i never tried it. any pointers?

--alex--

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Re: [Flightgear-devel] f16 speedbrakes

2008-09-06 Thread Fabian Grodek
On Fri, Sep 5, 2008 at 11:54 PM, Erik Hofman [EMAIL PROTECTED] wrote:

 
  I also see that (I'm only looking at the speedbrakes effects).
  Two things are unclear for me:
  1. The values of alpha in f16.xml are exactly half those in NASA's
  TP1538 report.
  2. The values of the coefficients are close to each other, but not
  exactly the same.
 
  For CmDsb I'm looking on TP1538 page 58 (PDF page 64)
  For CLDsb I'm looking on TP1538 page 65 (PDF page 71)

 Off course you need to transform the data from body axes to wind axes
 first..

 Erik


Sorry I've mixed the page numbers on TP1538 paper in my former message.
Erik,
1. Transformation from body to wind axes would modify the coefficient values
much more than the differences I see; moreover, I see difefrences even at
alpha=0 (for CmDsb, -0.0036 in f16.xml instead of -0.0038 in TP1538).
2. The alpha values are still HALF those on TP1538.

No matters what our conclusion will be on these issues, I really value the
great job you've done in this model, making it a great source for learning
JSBSim. Thanks.

Fabian
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Re: [Flightgear-devel] f16 speedbrakes

2008-09-06 Thread Alex Romosan
Jon S. Berndt writes:

 I don't know if this matters, but remember that not too long ago we
 added the ability to enter aero coefficients in several coordinate
 systems - including BODY and WIND, etc.

so if i were to represent the wind tunnel data in x,y,z axis then the
drag due to horizontal tail deflection (the data on pages 45-49 of the
nasa technical paper 1538) would then look like this:

axis name=X
  function name=aero/coefficient/CDDh
descriptionDrag_due_to_horizontal_tail_deflection/description
product
  propertyaero/qbar-psf/property
  propertymetrics/Sw-sqft/property
  table name=CDdHT
independentVar lookup=rowaero/beta-deg/independentVar
independentVar lookup=columnaero/alpha-deg/independentVar
independentVar lookup=tablefcs/elevator-pos-deg/independentVar
tableData breakPoint=-25
  -30 -25 -20 -15 -10 -8 -6 -4 -2 0 2 4 6 8 10 15 20 25 30 
  -20 -0.1837 -0.1853 -0.1904 -0.1899 -0.1949 -0.1914 -0.1872 -0.186 
-0.186 -0.1868 -0.1899 -0.1902 -0.19 -0.1896 -0.1883 -0.1833 -0.1838 -0.1787 
-0.1771
  -15 -0.1714 -0.1765 -0.1792 -0.1827 -0.1816 -0.1834 -0.1852 -0.1853 
-0.1877 -0.1875 -0.1898 -0.1876 -0.1868 -0.1848 -0.1841 -0.1852 -0.1817 -0.179 
-0.1739
  -10 -0.1531 -0.1627 -0.1692 -0.1718 -0.1695 -0.1693 -0.1707 -0.1735 
-0.1772 -0.1787 -0.1769 -0.1729 -0.1711 -0.1706 -0.1698 -0.1721 -0.1695 -0.163 
-0.1534
  -5 -0.1151 -0.1232 -0.1276 -0.1317 -0.139 -0.1415 -0.142 -0.1425 
-0.1437 -0.1432 -0.1425 -0.1422 -0.141 -0.1397 -0.1372 -0.1299 -0.1258 -0.1214 
-0.1133
  0 -0.0907 -0.0985 -0.1043 -0.1093 -0.112 -0.1115 -0.1122 -0.1124 
-0.113 -0.1132 -0.1129 -0.1119 -0.111 -0.1102 -0.1092 -0.1065 -0.1015 -0.0957 
-0.0879
  5 -0.0514 -0.0567 -0.0603 -0.064 -0.0653 -0.0661 -0.0668 -0.0675 
-0.069 -0.0693 -0.0686 -0.068 -0.0664 -0.065 -0.0649 -0.0631 -0.0594 -0.0558 
-0.0505
  10 -0.0079 -0.0108 -0.0099 -0.0101 -0.0074 -0.007 -0.0078 -0.009 
-0.0116 -0.012 -0.0123 -0.0106 -0.0088 -0.0083 -0.008 -0.0107 -0.0105 -0.0114 
-0.0085
  15 0.0354 0.0358 0.0388 0.0402 0.0477 0.0503 0.0535 0.0553 0.0538 
0.0537 0.0533 0.0536 0.0527 0.0509 0.0485 0.041 0.0396 0.0366 0.0362
  20 0.074 0.0756 0.0746 0.0745 0.0867 0.0888 0.0924 0.0941 0.0948 
0.0951 0.0975 0.0939 0.0913 0.0867 0.0824 0.0702 0.0703 0.0713 0.0697
  25 0.1092 0.1124 0.1102 0.1067 0.1101 0.1121 0.1126 0.1129 0.1123 
0. 0.1122 0.1125 0.1136 0.1115 0.1075 0.1041 0.1076 0.1098 0.1066
  30 0.0915 0.101 0.0975 0.1079 0.1188 0.1333 0.1399 0.1422 0.1443 
0.1435 0.1431 0.1407 0.1379 0.1359 0.1323 0.1214 0.111 0.1145 0.105
  35 0.1079 0.1137 0.1198 0.1278 0.1402 0.1425 0.1478 0.157 0.1623 
0.1663 0.1667 0.1664 0.1637 0.156 0.146 0.1336 0.1256 0.1195 0.1137
  40 0.1306 0.1437 0.135 0.1441 0.1574 0.1585 0.1601 0.1682 0.1726 
0.1739 0.1711 0.1699 0.1655 0.1611 0.1567 0.1434 0.1343 0.143 0.1299
  45 0.1535 0.1603 0.1605 0.1604 0.1637 0.1671 0.1664 0.1639 0.1674 
0.1659 0.1649 0.165 0.1625 0.1597 0.1573 0.154 0.1541 0.1539 0.1471
  50 0.1471 0.1584 0.1646 0.1671 0.1712 0.1712 0.1676 0.1644 0.1656 
0.1693 0.1714 0.1728 0.1749 0.1725 0.173 0.1537 0.1457 0.1435 0.1362
  55 0.1554 0.1615 0.1568 0.1661 0.1778 0.1769 0.1765 0.1749 0.1762 
0.1804 0.1743 0.1666 0.1677 0.1724 0.1761 0.1722 0.1347 0.1448 0.1442
  60 0.1501 0.1599 0.1647 0.1525 0.1664 0.1662 0.1704 0.171 0.1719 
0.1718 0.1728 0.173 0.1734 0.1721 0.1688 0.1471 0.1462 0.1486 0.146
  70 0.1501 0.1536 0.1569 0.142 0.1573 0.1595 0.1788 0.1715 0.1738 
0.1695 0.171 0.1712 0.173 0.172 0.1686 0.1474 0.1567 0.1557 0.1545
  80 0.1685 0.1615 0.1559 0.152 0.1521 0.1521 0.1535 0.1585 0.1566 
0.1598 0.1573 0.1563 0.1586 0.1558 0.1572 0.141 0.141 0.1467 0.1538
  90 0.1712 0.1651 0.1608 0.1648 0.1676 0.166 0.1686 0.1667 0.1669 
0.166 0.1672 0.1662 0.1664 0.1711 0.1677 0.1531 0.1493 0.1549 0.1624
/tableData
tableData breakPoint=-10
  -30 -25 -20 -15 -10 -8 -6 -4 -2 0 2 4 6 8 10 15 20 25 30 
  -20 -0.1362 -0.1351 -0.1419 -0.1386 -0.1374 -0.133 -0.1268 -0.1249 
-0.1222 -0.1223 -0.1246 -0.1247 -0.1252 -0.1257 -0.1282 -0.1294 -0.1327 -0.1259 
-0.127
  -15 -0.1216 -0.1245 -0.1235 -0.1208 -0.1176 -0.1176 -0.117 -0.1177 
-0.1184 -0.1188 -0.1185 -0.1187 -0.1182 -0.1178 -0.1184 -0.1216 -0.1243 -0.1253 
-0.1224
  -10 -0.1018 -0.1066 -0.1068 -0.1071 -0.1061 -0.1068 -0.1072 -0.1083 
-0.1094 -0.1147 -0.1095 -0.1084 -0.1077 -0.1063 -0.1069 -0.1079 -0.1076 -0.1074 
-0.1026
  -5 -0.0655 -0.0706 -0.0746 -0.0771 -0.0836 -0.0864 -0.0876 -0.0887 
-0.0889 -0.0893 -0.0885 -0.0875 -0.0859 -0.0842 -0.0812 -0.0747 -0.0722 -0.0682 
-0.0631
  0 -0.0483 -0.0509 -0.0532 -0.0544 -0.0578 -0.0589 -0.0597 -0.0606 
-0.0613 -0.0617 -0.0611 -0.0603 -0.0595 -0.0577 -0.0561 -0.0527 -0.0515 -0.0492 
-0.0466
  5 -0.0118 -0.0106 -0.0096 -0.0102 -0.0142 -0.0148 -0.0155 -0.0161 

Re: [Flightgear-devel] f16 speedbrakes

2008-09-05 Thread Fabian Grodek
On 9/4/08, Alex Romosan [EMAIL PROTECTED] wrote:

 Erik Hofman writes:

  Alex Romosan wrote:
  can you give me a pointer as to where i could get this data? thanks.
 
  Search for NASA Technical Paper 1538

 i've been looking at it but i can't figure out the relationship
 between the number in the report and the numbers in the flightgear
 model. if somebody could explain the magic involved i would really
 appreciate it. thanks.

 --alex--


I also see that (I'm only looking at the speedbrakes effects).
Two things are unclear for me:
1. The values of alpha in f16.xml are exactly half those in NASA's TP1538
report.
2. The values of the coefficients are close to each other, but not exactly
the same.

For CmDsb I'm looking on TP1538 page 58 (PDF page 64)
For CLDsb I'm looking on TP1538 page 65 (PDF page 71)

Ron?

Fabian
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Re: [Flightgear-devel] f16 speedbrakes

2008-09-05 Thread Erik Hofman
Fabian Grodek wrote:
 On 9/4/08, *Alex Romosan* [EMAIL PROTECTED] 
 mailto:[EMAIL PROTECTED] wrote:
 
 Erik Hofman writes:
 
   Alex Romosan wrote:
   can you give me a pointer as to where i could get this data? thanks.
  
   Search for NASA Technical Paper 1538
 
 i've been looking at it but i can't figure out the relationship
 between the number in the report and the numbers in the flightgear
 model. if somebody could explain the magic involved i would really
 appreciate it. thanks.
 
 --alex--
 
  
 I also see that (I'm only looking at the speedbrakes effects).
 Two things are unclear for me:
 1. The values of alpha in f16.xml are exactly half those in NASA's 
 TP1538 report.
 2. The values of the coefficients are close to each other, but not 
 exactly the same.
  
 For CmDsb I'm looking on TP1538 page 58 (PDF page 64)
 For CLDsb I'm looking on TP1538 page 65 (PDF page 71)

Off course you need to transform the data from body axes to wind axes 
first..

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-09-05 Thread Jon S. Berndt
 
 Of course you need to transform the data from body axes to wind axes
 first..
 
 Erik

I don't know if this matters, but remember that not too long ago we added
the ability to enter aero coefficients in several coordinate systems -
including BODY and WIND, etc.

Jon



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Re: [Flightgear-devel] f16 speedbrakes

2008-09-04 Thread Alex Romosan
Erik Hofman writes:

 Alex Romosan wrote:
 can you give me a pointer as to where i could get this data? thanks.
   
 Search for NASA Technical Paper 1538

i've been looking at it but i can't figure out the relationship
between the number in the report and the numbers in the flightgear
model. if somebody could explain the magic involved i would really
appreciate it. thanks.

--alex--

-- 
| I believe the moment is at hand when, by a paranoiac and active |
|  advance of the mind, it will be possible (simultaneously with  |
|  automatism and other passive states) to systematize confusion  |
|  and thus to help to discredit completely the world of reality. |

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-31 Thread Fabian Grodek
On 8/30/08, Erik Hofman [EMAIL PROTECTED] wrote:

  ... But I don't see any pitching moment effect; from
  what I see in NASA TP 1538 http://hdl.handle.net/2002/11034 I
  understand there is a pitch-down effect from the speedbrakes.
 
 It looks like you don't have the latest version of the configuration
 file, it's defined under CmDsb


I see. The current f16.xml version in JSBSim repository is 1.82, which
indeed has the CmDsb effect.
Nevertheless, the current f16.xml version in FlighGear is 1.44, which does
not contain the CmDsb component. Since this is a FlightGear mailing list, I
was looking only at the file on FG repository.
Fabian
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Re: [Flightgear-devel] f16 speedbrakes

2008-08-31 Thread Ron Jensen
On Sun, 2008-08-31 at 12:31 +0200, Fabian Grodek wrote:
 On 8/30/08, Erik Hofman [EMAIL PROTECTED] wrote: 
  ... But I don't see any pitching moment effect; from
  what I see in NASA TP 1538
 http://hdl.handle.net/2002/11034 I
  understand there is a pitch-down effect from the
 speedbrakes.
 
 It looks like you don't have the latest version of the
 configuration
 file, it's defined under CmDsb
  
 I see. The current f16.xml version in JSBSim repository is 1.82, which
 indeed has the CmDsb effect.
 Nevertheless, the current f16.xml version in FlighGear is 1.44, which
 does not contain the CmDsb component. Since this is a FlightGear
 mailing list, I was looking only at the file on FG repository.
 Fabian

Fabian,

Version 1.44 is the release version.  It has had many updates since then
and is currently at version 1.62
http://cvs.flightgear.org/viewvc/data/Aircraft/f16/f16.xml?view=logpathrev=HEAD


Ron



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Re: [Flightgear-devel] f16 speedbrakes

2008-08-30 Thread Erik Hofman


Alex Romosan wrote:
 can you give me a pointer as to where i could get this data? thanks.
   
Search for NASA Technical Paper 1538

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-30 Thread Erik Hofman


Fabian Grodek wrote:
  
 Erik,
 In the F16 aero config file I see there's indeed an increase in lift 
 for certain speedbrakes deflection, accompanied by the expected huge 
 increase in drag. But I don't see any pitching moment effect; from 
 what I see in NASA TP 1538 http://hdl.handle.net/2002/11034 I 
 understand there is a pitch-down effect from the speedbrakes.

It looks like you don't have the latest version of the configuration 
file, it's defined under CmDsb

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-30 Thread Alex Romosan
Erik Hofman writes:

 Alex Romosan wrote:
 can you give me a pointer as to where i could get this data? thanks.
   
 Search for NASA Technical Paper 1538

thanks.

--alex--

-- 
| I believe the moment is at hand when, by a paranoiac and active |
|  advance of the mind, it will be possible (simultaneously with  |
|  automatism and other passive states) to systematize confusion  |
|  and thus to help to discredit completely the world of reality. |

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-29 Thread Erik Hofman
Alex Romosan wrote:

 i hate to bring this up again but i still think the speedbrakes don't
 work as they should, instead generating quite a lot of lift. i've
 tested this on final approach at about 160-170 knots, speedbrakes on;
 i can keep the plane level. retract the speedbrakes, the plane starts
 descending really fast (the nose position doesn't change). open the
 speed brakes, the plane goes climbing. again this is with the engine
 at idle and at very slow speeds.

Believe me, this is correct behavior, and this is why:

The fuselage sections on either side, between the the engine compartment 
(the round tube) and the wing root are good for 15% to 25% of the 
generated lift. Get them wrong on RC controlled model airplanes and it 
won't even fly properly (I know this from second hand experience).

Now, if you deploy the speedbrakes the lower clamp shell acts exactly 
like a flap at the rear end of the wing. If it weren't for the presence 
of the upper clamp shell, it wouldn't even produce much drag.

I can assure you; it is modeled correctly now.

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-29 Thread Alex Romosan
Erik Hofman writes:

 Believe me, this is correct behavior, and this is why:

i found a nice article about flying in an f16:

  http://www.avweb.com/news/skywrite/181916-1.html

this is the part about the speed brakes:

  Here's where the speed brakes come in handy, I'll open em up. And
  you'll see what happens.

  I felt what happens! It seemed my face was being pulled from my
  skull. I couldn't believe how effective those speed brakes were. An
  F-16's speed brakes are located at the back of the fuselage either
  side of the engine nacelle, and really look diminutive. However,
  introducing even that much surface area to hang out in the 600-mph
  breeze has a pronounced effect on one's forward motion. We slowed to
  about 400 then he retracted the brakes and let the airspeed start
  increasing again.

--alex--

-- 
| I believe the moment is at hand when, by a paranoiac and active |
|  advance of the mind, it will be possible (simultaneously with  |
|  automatism and other passive states) to systematize confusion  |
|  and thus to help to discredit completely the world of reality. |

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-29 Thread Erik Hofman
Alex Romosan wrote:
 Erik Hofman writes:
 
 Believe me, this is correct behavior, and this is why:
 
 i found a nice article about flying in an f16:
 
   http://www.avweb.com/news/skywrite/181916-1.html
 
 this is the part about the speed brakes:
 
   Here's where the speed brakes come in handy, I'll open em up. And
   you'll see what happens.
 
   I felt what happens! It seemed my face was being pulled from my
   skull. I couldn't believe how effective those speed brakes were. An
   F-16's speed brakes are located at the back of the fuselage either
   side of the engine nacelle, and really look diminutive. However,
   introducing even that much surface area to hang out in the 600-mph
   breeze has a pronounced effect on one's forward motion. We slowed to
   about 400 then he retracted the brakes and let the airspeed start
   increasing again.

This says nothing about generating lift or not..

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-29 Thread Alex Romosan
Erik Hofman writes:

 Alex Romosan wrote:

   I felt what happens! It seemed my face was being pulled from my
   skull. I couldn't believe how effective those speed brakes were. An
   F-16's speed brakes are located at the back of the fuselage either
   side of the engine nacelle, and really look diminutive. However,
   introducing even that much surface area to hang out in the 600-mph
   breeze has a pronounced effect on one's forward motion. We slowed to
   about 400 then he retracted the brakes and let the airspeed start
   increasing again.

 This says nothing about generating lift or not..

no, but it would seem to indicate that the speed brakes are quite
effective at slowing down the aircraft which is not at all the case
with the current model in flightgear.

and nothing to do with the speed brakes, but this is a really cool
video of an f16 dead stick landing:

  http://www.patricksaviation.com/videos/SUPERGT/3384

--alex--

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-29 Thread gerard robin
On ven 29 août 2008, Erik Hofman wrote:
 Alex Romosan wrote:
  Erik Hofman writes:
  Believe me, this is correct behavior, and this is why:
 
  i found a nice article about flying in an f16:
 
http://www.avweb.com/news/skywrite/181916-1.html
 
  this is the part about the speed brakes:
 
Here's where the speed brakes come in handy, I'll open em up. And
you'll see what happens.
 
I felt what happens! It seemed my face was being pulled from my
skull. I couldn't believe how effective those speed brakes were. An
F-16's speed brakes are located at the back of the fuselage either
side of the engine nacelle, and really look diminutive. However,
introducing even that much surface area to hang out in the 600-mph
breeze has a pronounced effect on one's forward motion. We slowed to
about 400 then he retracted the brakes and let the airspeed start
increasing again.

 This says nothing about generating lift or not..

 Erik


 Only my 2 cents, if the question is not stupid :)
How does  the fly-by-wire,  regarding the speedbrake lift effect ?

Regards

BTW: An other AC the F15 should have a negative lift with speedbrake



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J'ai décidé d'être heureux parce que c'est bon pour la santé. 
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Re: [Flightgear-devel] f16 speedbrakes

2008-08-29 Thread Erik Hofman
gerard robin wrote:

 A Only my 2 cents, if the question is not stupid :)
 How does  the fly-by-wire,  regarding the speedbrake lift effect ?

What happens (with regard to the fly-by-wire system) is this:

Speedbrake deflection causes a pitching moment which the FCS 
automatically compensates because there is no pitching moment requested 
by the pilot.

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-29 Thread Erik Hofman
Alex Romosan wrote:
 Erik Hofman writes:
 
 Alex Romosan wrote:
   I felt what happens! It seemed my face was being pulled from my
   skull. I couldn't believe how effective those speed brakes were. An
   F-16's speed brakes are located at the back of the fuselage either
   side of the engine nacelle, and really look diminutive. However,
   introducing even that much surface area to hang out in the 600-mph
   breeze has a pronounced effect on one's forward motion. We slowed to
   about 400 then he retracted the brakes and let the airspeed start
   increasing again.
 This says nothing about generating lift or not..
 
 no, but it would seem to indicate that the speed brakes are quite
 effective at slowing down the aircraft which is not at all the case
 with the current model in flightgear.

Sorry, I got the data from windtunnel test data performed by NASA. I 
tend to believe that over a first time experience from some one claiming 
he has had the time of his life.

So until somebody can show me what exactly is wrong I won't change it 
and won't let anybody else make changes to it.

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-29 Thread Alex Romosan
Erik Hofman writes:

 Sorry, I got the data from windtunnel test data performed by NASA.

can you give me a pointer as to where i could get this data? thanks.

--alex--

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-14 Thread Erik Hofman

Ok, I think I have most of it figured out. I might even consider 
upgrading the status to 'production' the way it is now.

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-14 Thread Alex Romosan
Erik Hofman writes:

 Ok, I think I have most of it figured out. I might even consider 
 upgrading the status to 'production' the way it is now.

hmm, i don't know how the real f-16 behaves but i still find the
current behaviour a bit strange. level flight, ~350 knots extend the
brakes the aircraft pitches up slightly and really starts to climb (no
effect on the speed at all). push the nose down (quite a lot) to bring
it back to level flight speed actually increases. not very useful if
you are actually trying to slow down.

--alex--

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-14 Thread Erik Hofman
Alex Romosan wrote:
 hmm, i don't know how the real f-16 behaves but i still find the
 current behaviour a bit strange. level flight, ~350 knots extend the
 brakes the aircraft pitches up slightly and really starts to climb (no
 effect on the speed at all). push the nose down (quite a lot) to bring
 it back to level flight speed actually increases. not very useful if
 you are actually trying to slow down.
   
I have checked the data three times to see if I was doing something 
wrong, but unless someone mixed up the tables in the wind tunnel data 
report got this is how it should behave. I do know that it actually does 
reduce airspeed (albeit a little) with 7.5 degree pitch down at final 
approach, Which sounds about right to me.

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-14 Thread Erik Hofman

Ok, tested it again. The only way I could reproduce your scenario is not 
to have the throttle near idle.
As I did state earlier, the speeedbrakes of the F-16 are quite small and 
as it turns out the engine can easily produce enough thrust to overcome 
the increased drag.

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-14 Thread Alex Romosan
Erik Hofman writes:

 Ok, tested it again. The only way I could reproduce your scenario is not 
 to have the throttle near idle.
 As I did state earlier, the speeedbrakes of the F-16 are quite small and 
 as it turns out the engine can easily produce enough thrust to overcome 
 the increased drag.

yes, the throttle was nowhere near idle. thanks for the great work.

--alex--

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-12 Thread Alex Romosan
Erik Hofman writes:

 You were right, I had to map speedbrake-pos-norm to 
 speedbrake-pos-rad/deg by using an aerosurface scale section.

i think there is still something wrong with the speedbrakes but i am
not sure how to quantify this. basically i think they provide way too
much lift (which makes me suspect there is a sign problem somewhere).
the effect is more pronounced at slower speeds (250 - 300 knots or
so). extend the speedbrakes and see the f16 suddenly start climbing.
handy if you are too low on approach but not realistic at all (i would
expect the speedbrakes to cause the plane to lose altitude faster not
provide lift).

--alex--

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-12 Thread Erik Hofman


Alex Romosan wrote:
 i think there is still something wrong with the speedbrakes but i am
 not sure how to quantify this. basically i think they provide way too
 much lift (which makes me suspect there is a sign problem somewhere).
 the effect is more pronounced at slower speeds (250 - 300 knots or
 so). extend the speedbrakes and see the f16 suddenly start climbing.
 handy if you are too low on approach but not realistic at all (i would
 expect the speedbrakes to cause the plane to lose altitude faster not
 provide lift).
Correct, in fact it's creating a downpitching moment that is 
overcompensated with the current setup.
I'm still working on this.

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-01 Thread Erik Hofman
Alex Romosan wrote:
 i noticed that on the f16 the speedbrakes have no effect at all and i
 managed to track it down to the fact that the various coefficients use
 fcs/mag-speedbrake-pos-rad on input which never gets set anywhere (so
 it is always 0).
 
 digging through the cvs logs i found that in version 1.17 of f16.xml
 the output of fcs/speedbrake-cmd-norm used to be fcs/speedbrake-pos-rad
 and it was set to 1.05 (which would translate roughly to 60 degrees).
 so i tried applying this patch:

 now the various coefficients change when i activate the speedbrake but
 there is still no noticeable effect on the plane.
 
 does anybody have any ideas how to fix the speedbrakes?

Looking at the code it looks like setting speed-break-pos-norm should be 
the same as setting speed-break-pos-rad so the patch shouldn't have any 
effect.

I think you expect too much effect from the speedbrakes, they are quite 
small for the F-16 and can be deployed in-flight without any problems 
(in fact, they tend to get used during the complete final approach cycle 
over here).

Try diving without any power (throttle to nil) with the speedbrakes 
deployed for a while and then retract them. If all works well you will 
see the speed increase.

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-01 Thread Alex Romosan
Erik Hofman writes:

 Looking at the code it looks like setting speed-break-pos-norm should be 
 the same as setting speed-break-pos-rad so the patch shouldn't have any 
 effect.

look at aero/coefficient/CDDsb or fcs/mag-speedbrake-pos-rad in the
property browser. when you deploy the speed brakes the values are
still zero (they never change).

and i looked at the code speed-break-pos-norm never sets
speed-break-pos-rad (it couldn't really, what would be the
correlation).

--alex--

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-01 Thread Erik Hofman
Alex Romosan wrote:
 Erik Hofman writes:
 
 Looking at the code it looks like setting speed-break-pos-norm should be 
 the same as setting speed-break-pos-rad so the patch shouldn't have any 
 effect.
 
 look at aero/coefficient/CDDsb or fcs/mag-speedbrake-pos-rad in the
 property browser. when you deploy the speed brakes the values are
 still zero (they never change).
 
 and i looked at the code speed-break-pos-norm never sets
 speed-break-pos-rad (it couldn't really, what would be the
 correlation).

I just tested it and it seems have less effect than I expected. hmm.
Have to look at it some more.

Both are affected when one or the other is changed since they are tied 
using the property manager to the proper function in 
JSBSim/models/FGFCS.cpp which sets the same internal variable.

Erik

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Re: [Flightgear-devel] f16 speedbrakes

2008-08-01 Thread Erik Hofman
Alex Romosan wrote:
 Erik Hofman writes:
 
 Looking at the code it looks like setting speed-break-pos-norm should be 
 the same as setting speed-break-pos-rad so the patch shouldn't have any 
 effect.
 
 look at aero/coefficient/CDDsb or fcs/mag-speedbrake-pos-rad in the
 property browser. when you deploy the speed brakes the values are
 still zero (they never change).

You were right, I had to map speedbrake-pos-norm to 
speedbrake-pos-rad/deg by using an aerosurface scale section.

Thanks for the hints.

Erik

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[Flightgear-devel] f16 speedbrakes

2008-07-31 Thread Alex Romosan
i noticed that on the f16 the speedbrakes have no effect at all and i
managed to track it down to the fact that the various coefficients use
fcs/mag-speedbrake-pos-rad on input which never gets set anywhere (so
it is always 0).

digging through the cvs logs i found that in version 1.17 of f16.xml
the output of fcs/speedbrake-cmd-norm used to be fcs/speedbrake-pos-rad
and it was set to 1.05 (which would translate roughly to 60 degrees).
so i tried applying this patch:

--- f16.xml 18 Jul 2008 14:41:41 -  1.50
+++ f16.xml 31 Jul 2008 20:22:09 -
@@ -572,6 +572,12 @@
 outputfcs/speedbrake-pos-norm/output
 /kinematic
 
+   pure_gain name=Speedbrake Deflection
+   inputfcs/speedbrake-pos-norm/input
+   gain60./gain
+   outputfcs/speedbrake-pos-deg/output
+   /pure_gain
+
 /channel
 
 channel name=Landing Gear

now the various coefficients change when i activate the speedbrake but
there is still no noticeable effect on the plane.

does anybody have any ideas how to fix the speedbrakes?

--alex--

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