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#1
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I was flying up to Bridgeport Texas on Tuesday and tried to get away from a 20kt headwind. So I took the MTO over broken clouds at over 8000 feet and 95kts.
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#2
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How small/narrow gets the seat at this hight, Texasautogyro?
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Giorgos Cyprus http://www.aviomania.com/ Visit Aviomania Aircraft Webpage [url]http://www.youtube.com/watch?v=6QRZb- Last edited by scandtours; 09-23-2011 at 03:23 AM. |
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#3
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I took my Bensen to 5000agl once. It felt mighty small, and it was a really lonely feeling.
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David McCutchen615-390-2228 |
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#4
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I am confused at how conditions change with altitude. With 20 mph headwind, how would you know to look for calmer conditions when climbing? Doesn't winds aloft increase with altitude or does getting above the clouds change things? I would like to learn how to make more effective cross countries and work with weather better. Or work against it I should say. Thanks for your advice.
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BRIAN WILLIS Sport Pilot, Gyroplane Pace, Florida RAF 2000 GTX SE FI (N429RK) Stabilator/Stability Dust Maule MT7-235 (N235) Got STOL? Building the GENESIS G1sa - Aviomania YouTube Videos |
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#5
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Get the winds aloft conditions and forecast. Sometimes, there is no wind at some altitudes. That's why Airlines will pick altitudes during their route to reduce the travel time and that is the secret sauce for hot air balloners and how they change directions by changing altitudes.
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#6
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Desmon and I were flying my RAF one day and the wind was rough and choppy, we took it up to 3,000, just above the clouds, and it was unbelievably smooth.
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Mike Grosshans PRA #41496 PRA Chapter 62 Secretary Southwest Rotorcraft Editor RAF Pilots Association www.gyrosaway.com www.gyroplanevideos.com |
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#7
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The winds aloft forecast would give a lot of useful info at different altitudes. If the machine has the capability of climbing, it is great to find an altitude with tail winds based on the charts.
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Antony Thomas |
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#8
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@Brian
Hi Buddy!!! Here is a detailed answer: The wind changes direction as you increase or decrease in altitude. With hot air balloons you drop bird seed to see where the wind is blowing below you to find the air current going in the direction you wish to fly. When flying fixed wing aircraft the winds aloft forecast can a big difference in the time required to make the flight. I have had a 100+ tail wind on several occasions - now that a fast/short flight. Here is an example of today’s winds aloft forecast for San Diego. FT 3000 6000 9000 12000 18000 24000 30000 34000 39000 SAN 9900 1715+20 1520+13 1325+06 1525-12 1823-24 233138 244046 243954 The FT = the altitude of the wind/ Flight level. 3000= 3000 feet, 18000 = 18000 feet, etc. At 3000 feet it say’s 9900 = the wind direction is 99° and the wind speed is 0 K. At 6000 feet is says 1715+20 = 17 add a 0 = 170° wind direction, the 15 is the speed in knots and the +20 is the temperature. The temperature is provided so I can calculate TRUE air speed at that altitude. How we use it: So, I need to plan a flight to El Mirage and must fly at an even attitude +500 feet for my VFR required heading of 329°. . I also must fly at 8,500 feet or above to fly over the controlled airspace of Los Angles controlled airspace. I wish to find an altitude with the best tail-wind = the one coming closes to my heading of 329°. So for my flight what altitude should I fly at for the best ground speed possible? ==== Here is one more piece of the puzzle: Because all values are not listed on the tables or graphs, interpolation is often required to determine intermediate values for a particular flight condition or performance situation. Interpolation To interpolate means to compute intermediate values between a series of given values. In many instances when performance is critical, an accurate determination of the performance values is the only acceptable means to enhance safe flight. Guessing to determine these values should be avoided. Interpolation is simple to perform if the method is understood. The following are examples of how to interpolate or accurately determine the intermediate values between a series of given values. The numbers in column A range from 10 to 30 and the numbers in column B range from 50 to 100. Determine the intermediate numerical value in column B that would correspond with an intermediate value of 20 placed in column A. A B 10 50 20 X = Unknown 30 100 It can be visualized that 20 is halfway between 10 and 30; therefore, the corresponding value of the unknown number in column B would be halfway between 50 and 100, or 75.
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Resistance is futile…… You will be compiled! ![]() Cheers, John Rountree ![]() PRA- Webmaster and Volunteer Coordinator U.S. Agent for Aviomania Aircraft See: Aviomania USA http://www.AviomaniaUSA.com Last edited by All_In; 09-23-2011 at 07:02 AM. |
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#9
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Quote:
-- Chris.
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Read about my trip across the USA in an MT03 gyro here. |
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#10
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Wasn't 99 86's partner?
Graeme.
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Red meat is not bad for you Fuzzy green meat is bad for you. |
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#11
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Thanks so much for that John. I read winds aloft completely wrong then. I thought that the +20 was wind speed and that it was a constant direction all the way up. Now I understand that the direction changes as you change altitude. I need a course in what you are talking about. Some good CC training.
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BRIAN WILLIS Sport Pilot, Gyroplane Pace, Florida RAF 2000 GTX SE FI (N429RK) Stabilator/Stability Dust Maule MT7-235 (N235) Got STOL? Building the GENESIS G1sa - Aviomania YouTube Videos |
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#12
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Use can a free website like www.navmonster.com to confirm your interpretation. They reformat the code to be very understandable.
Here is another nice site: http://www.usairnet.com/cgi-bin/Wind...course=azimuth Last edited by SpyderMike; 09-23-2011 at 09:44 AM. |
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#13
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If you were west bound low altitude then ~2000 ft would be a good altitude to choose..
Code:
Forecast high taken from DFW
23-SEP-2011 12 UTC Soaring report from FWD upper air data.
Forecast high: 82 F; est. base of any clouds: 5500 feet AGL.
=== Raw Upper-Air Data ===
Feet MSL: 643 1063 1780 2661 2900 2931 3662 3942 4226 5093
Pres mb: 998 983 958 928 920 919 895 886 877 850
Temp C: 12.8 14.6 14.4 12.6 12.8 13.4 13.2 14.8 15.4 14.8
VirT C: 14.4 16.5 16.3 14.3 14.4 15.0 14.4 15.5 15.8 15.1
DewPt C: 12.2 14.6 14.4 12.2 11.6 11.2 7.2 -1.2 -7.6 -13.2
Wdir@kts: 30 7 330 7
=== Interpolations (temps in deg. F, altitudes in feet MSL) ===
MSL *TI* Wdir@kts trig VirT 2.3 degrees/division ("`": Dry Adiabatic)
----- ---- -------- ---- . ---- -----------------------------------------
18000 13.8 107 | 17.3 ` :
17500 13.3 106 | 19.1 ` :
17000 12.9 105 | 21.0 ` :
16500 12.4 104 | 22.8 ` :
16000 11.7 360 23 103 | 24.2 ` :
15500 10.8 101 | 25.3 ` :
15000 10.4 101 | 27.2 ` :
14500 10.3 100 | 29.7 ` :
14000 10.2 340 14 100 | 32.2 ` :
13500 10.1 100 | 34.6 ` :
13000 10.0 100 | 37.1 ` :
12500 9.7 99 | 39.2 ` :
12000 9.1 340 18 98 | 40.8 ` :
11500 8.4 97 | 42.3 ` :
11000 7.7 96 | 43.8 ` :
10500 7.1 310 11 95 | 45.3 ` :
10000 6.3 93 | 46.6 ` :
9500 5.5 92 | 47.8 ` :
9000 4.7 295 12 90 | 49.0 ` :
8500 3.8 89 | 50.2 ` :
8000 3.0 305 19 87 | 51.4 ` :
7500 2.2 86 | 52.6 ` :
7000 1.4 310 15 84 | 53.8 `:
6500 0.6 83 | 55.0 :
6000 -0.1 305 13 82 | 56.5 :
5500 -0.3 82 | 58.7 :
5000 -1.5 330 7 80 | 59.3 :`
4500 -2.5 78 | 60.1 : `
4000 -4.0 355 6 76 | 60.0 : `
3500 -6.5 71 | 58.2 : `
3000 -7.6 10 8 69 | 58.9 : `
2500 -9.4 66 | 58.4 : `
2000 -9.8 80 7 65 | 60.4 : `
1500 -10.7 64 | 61.4 : `
1000 -12.4 61 | 61.1 : `
=== Complete Upper Air Data ===
P(mb) H(ft) Tv(C) T(C) DP(C) wind dir wind spd
998.0 643 14.4 12.8 12.2
983.0 1063 16.5 14.6 14.6
958.0 1780 16.3 14.4 14.4
928.0 2661 14.3 12.6 12.2
920.0 2900 14.4 12.8 11.6 30 7
919.0 2931 15.0 13.4 11.2
895.0 3662 14.4 13.2 7.2
886.0 3942 15.5 14.8 -1.2
877.0 4226 15.8 15.4 -7.6
850.0 5093 15.1 14.8 -13.2 330 7
843.0 5322 15.3 15.0 -15.0
817.0 6187 13.2 13.0 -20.0
700.0 10397 7.6 7.4 -22.6 310 11
657.0 12098 4.8 4.6 -23.4
642.0 12714 3.6 3.4 -18.6
582.0 15289 -3.5 -3.7 -19.7
559.0 16332 -4.7 -4.9 -23.9
500.0 19177 -10.6 -10.7 -34.7 350 26
492.0 19583 -11.4 -11.5 -35.5
400.0 24666 -23.7 -23.7 -50.7 320 19
300.0 31326 -40.5 -40.5 -64.5 305 24
275.0 33249 -45.7 -45.7 -65.7
250.0 35314 -49.7 -49.7 -67.7 285 31
231.0 36996 -53.7 -53.7 -69.7
220.0 38022 -54.9 -54.9 -69.9
216.0 38406 -54.9 -54.9 -69.9
213.0 38701 -53.7 -53.7 -69.7
200.0 40022 -55.7 -55.7 -70.7 280 45
196.0 40444 -56.5 -56.5 -71.5 280 46
189.0 41202 -55.5 -55.5 -70.5
181.0 42104 -57.1 -57.1 -71.1
174.0 42925 -55.9 -55.9 -70.9
155.0 45326 -58.1 -58.1 -72.1
152.0 45730 -57.7 -57.7 -71.7
150.0 46004 -58.1 -58.1 -72.1 280 52
122.0 50224 -63.1 -63.1 -75.1
113.0 51773 -62.3 -62.3 -75.3
102.0 53829 -66.1 -66.1 -78.1 270 38
Additional wind data:
H(ft) dir spd
------ --- ---
2000 80 7
3000 10 8
4000 355 6
6000 305 13
7000 310 15
8000 305 19
9000 295 12
12000 340 18
14000 340 14
16000 360 23
20000 345 30
24000 320 20
25000 320 18
27000 325 14
29000 325 22
30000 315 23
31000 305 22
34000 310 29
35000 285 33
38000 290 44
39000 275 41
44000 270 58
49000 275 54
50000 270 45
52000 265 32
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Private Pilot Airplane Single Engine Land Private Pilot Airplane Single Engine Sea Private Pilot Airplane Multi Engine Land Private Pilot Glider Private Pilot Helicopter Private Pilot Gyroplane Instrument Ground Instructor Advanced Ground Instructor Airframe & Powerplant Mechanic |
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#14
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Here is something else glider pilots use, it's called Soar forecast....
http://www.soarforecast.com/ti.cgi?S...Altitude=18000 It has winds aloft and the altitudes where you can expect lift (thermal Turbulence) the bigger the negative TI # the more lift you should find.
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Private Pilot Airplane Single Engine Land Private Pilot Airplane Single Engine Sea Private Pilot Airplane Multi Engine Land Private Pilot Glider Private Pilot Helicopter Private Pilot Gyroplane Instrument Ground Instructor Advanced Ground Instructor Airframe & Powerplant Mechanic |
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