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#511
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"Fly a steady heading" --- not so easy.
Depends on prevailing wind strength and direction, both of which may be variable. The actual heading of the aircraft may not be the same as the resultant course flown. |
#512
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If you have visual references you'ld be quicker ploting your bearing from the NDB onto your map and looking for landmarks along that line. Using dead reconing you should have some idea where abouts ont the map you are (unless you get caught up in a furball and get completely lost. Of course you could always get your longitude using your aviation sextant and see where that intersects your bearing from the NDB. Though it depends how accurate you want to be. Cheers Last edited by Skoshi Tiger; 03-21-2010 at 11:54 AM. |
#513
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You guys are really trying to take all the fun out of this aren't you?
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![]() Personally speaking, the P-40 could contend on an equal footing with all the types of Messerschmitts, almost to the end of 1943. ~Nikolay Gerasimovitch Golodnikov |
#514
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![]() The range from aircraft to beacon (at both points of measurement) becomes known by using the law of sines. We have all three angles known in the triangle and we know one side (the distance traveled between the measurements). Quote:
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![]() The lower the wind and the higher the aircraft speed, the more accurate it should be, right? Because the ratio will determine how much movement was from aircraft and how much was wind affected. Assuming we don't have a grip on the wind.[/QUOTE] Quote:
![]() Question to all - is there any way of seeing how the wind is blowing relative to the aircraft? Both when seeing the ground (not having a map to compare to) and when flying without any visual on the ground. How did people figure this out in flight way up there? |
#515
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If one sees the ground normally one can use landmarks to estimate position. No ground visibility = no landmarks and no way to determine the drift. Over the sea at night, if visibility was good, bomber crews used to launch a flare with the rear gunner aiming at it from a distance. Regards, Insuber |
#516
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MikkOwl wrote
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#517
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MikkOwl is on right track here, but I think that normal triangulation procedure with single NDB would be following:
1. turn so that your plane is perpendicular to NDB. (NDB is at 270 or 90). 2. start watch and fly at constant speed maintaining the current heading. 3. stop watch when NDB bearing has changed 5 dec. 3. calculate distance flown during this time. 4. calculate distance to beacon. (distance flown/sin 5) For example if we fly at 300km/h TAS for 135 seconds. ((300/3.6)x135)/sin5) = 129km. So the beacon is 129 km away. I'm not 100% sure about the formula. I just did a quick scribbling on pen & paper. And this is without any wing correction.
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![]() Last edited by Viikate; 03-21-2010 at 05:57 PM. |
#518
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A lot of things are possible, but unless you're flying as a dedicated navigator you probably won't use most of it. It's not wrong, it's just not practical enough.
Whenever i dabble into stuff like that, i never do trigonometry. If i need to fly perpendicular to the beacon to obtain a distance fix, then it's clear i'm going off course to get a fix. Much better and faster to tune a second beacon and see where the lines intersect on the map, presto, you have a precise fix of your position. Even if your plane doesn't have a second nav radio and a second ADF, you can tune the first beacon and draw the line, then tune the second one and do the same on your single radio. Unless you are very close to the beacon (where the bearing changes fast), it will be accurate enough. There's lots of quick and dirty methods that give you enough accuracy without having to go all mathematical about it. For me, being able to obtain an accuracy equal to the visual range is good enough. For example, if the visibility at my current altitude and weather conditions is 10 miles, i won't mind at all if my radio navigation gives me a 5 mile error margin (it's actually lower than that most of the times, think 2-3 miles). And if flying at night, most aircraft that historically did it were better equipped to deal with it. Tuning 2 beacons and getting the respective bearings can also help you determine wind drift. See where the bearing lines cross and that's your position, wait (the 3m 15sec rule from silent hunter is good here) and get a new fix. Connect them on the map and it you used a 3m15s interval, the amount of kms travelled times 10 will give you your ground speed in knots. For example, if you've travelled 10km then your ground speed is 100 knots. Compare the heading of the line connecting the two fixes on the map with your actuall compass readout and you can also see the amount of wind drift involved. Some aircraft might also have specialized equipment. In B17 the mighty 8th, the navigator had a scope that looked down towards the ground. It had some continuous horizontal lines running across the scope view, as well as dotted lines that could be rotated. The idea was to rotate the dotted line lens until the view seemed to be moving without any drift (it's been a few years, don't remember it exactly), then you could read out the drift from the markings on the wheel that turned the dotted lines. |
#519
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d_NDB = (v_TAS * t_flight) / (3600 * sin( delta_angle ) ) where: d_NDB = distance to the beacon; v_TAS = true air speed (as Viikate said, not corrected for wind); t_flight = time in second; delta_angle = variation of heading; This formula is valid also for non metric units;
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#520
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http://www.nasm.si.edu/collections/a...d=A19500075025 Here's one with all the bits: http://cgi.ebay.com/ebaymotors/Bendi...-/360240715244 Here's the B-5: http://www.questmasters.us/sitebuild...er-423x366.jpg Last edited by Hoverbug; 03-21-2010 at 10:32 PM. |
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