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 Mach Number Characteristics
 Novice From United Kingdom, joined Aug 2012, 90 posts, RR: 0Posted Fri Oct 12 2012 10:50:22 UTC (3 years 4 months 3 days 17 hours ago) and read 8783 times:

 "Mach number is used as a speed reference at high altitudes, usually above 26000 ft, because the MN becomes the aircraft's limiting speed in preference to IAS. That is, up to approximately 26000 ft, an aircraft will climb at a constant IAS against an increasing MN, where the MN speed reaches the aircraft's MN limiting speed. Then above 26000 ft the aircraft is flown at a constant MN with a decreasing IAS for an increase in altitude." From the above i take it that the mach number limiting speed is the mach number speed that you reach when you change from IAS to MN? I would i also to right in saying when you are climbing at a constant IAS to 26000 ft your TAS would always have to be increasing due to ram air affects and also the density becoming less meaning you would have to fly faster to keep the indicated airspeed constant? Cheers
 DashTrash From United States of America, joined Aug 2006, 1646 posts, RR: 2 Reply 1, posted Fri Oct 12 2012 11:55:05 UTC (3 years 4 months 3 days 16 hours ago) and read 8759 times:

 Quoting Novice (Thread starter):From the above i take it that the mach number limiting speed is the mach number speed that you reach when you change from IAS to MN?

Not exactly sure how to answer that, but in practice you climb at an IAS until you reach your mach number specified in the profile.

Standard for us in my last airplane was 300 KTS above 10K, transition to M.80. If you flew it in VNAV, the aircraft would pitch for 300 until 300 was .8, then it would hold .8 all the way up until level off where it would accelerate closer to Mmo.

 Quoting Novice (Thread starter):I would i also to right in saying when you are climbing at a constant IAS to 26000 ft your TAS would always have to be increasing due to ram air affects and also the density becoming less meaning you would have to fly faster to keep the indicated airspeed constant?

Yep. TAS increases as you climb at a constant indicated airspeed.

 vikkyvik From United States of America, joined Jul 2003, 11908 posts, RR: 24 Reply 2, posted Fri Oct 12 2012 18:00:49 UTC (3 years 4 months 3 days 10 hours ago) and read 8662 times:

 Quoting Novice (Thread starter):From the above i take it that the mach number limiting speed is the mach number speed that you reach when you change from IAS to MN?

Whatever Mach number you end up climbing at likely won't be a limiting speed (that is, it wont' be Mmo or Md or anything). It might be your best climb Mach number, for efficiency, or climb rate, or whatever.

 Quoting Novice (Thread starter):I would i also to right in saying when you are climbing at a constant IAS to 26000 ft your TAS would always have to be increasing due to ram air affects and also the density becoming less meaning you would have to fly faster to keep the indicated airspeed constant?

Yes, but there is also less drag the higher you go, so it takes less thrust to fly higher. Point being, you don't necessarily have to keep increasing thrust to fly faster as you get higher.

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 BMI727 From United States of America, joined Feb 2009, 16559 posts, RR: 27 Reply 3, posted Fri Oct 12 2012 18:05:25 UTC (3 years 4 months 3 days 10 hours ago) and read 8661 times:

 Quoting vikkyvik (Reply 2):Yes, but there is also less drag the higher you go, so it takes less thrust to fly higher. Point being, you don't necessarily have to keep increasing thrust to fly faster as you get higher.

Thrust lapse often eats up the drag reduction.

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 Mir From United States of America, joined Jan 2004, 22657 posts, RR: 55 Reply 4, posted Fri Oct 12 2012 19:26:21 UTC (3 years 4 months 3 days 9 hours ago) and read 8639 times:

 Quoting Novice (Thread starter):I would i also to right in saying when you are climbing at a constant IAS to 26000 ft your TAS would always have to be increasing due to ram air affects and also the density becoming less meaning you would have to fly faster to keep the indicated airspeed constant?

It's not really a matter of having to fly faster - you just maintain the same IAS (just like you normally would) and your TAS ends up being faster as you climb all on its own.

-Mir

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 vikkyvik From United States of America, joined Jul 2003, 11908 posts, RR: 24 Reply 5, posted Sat Oct 13 2012 02:18:49 UTC (3 years 4 months 3 days 2 hours ago) and read 8573 times:

 Quoting BMI727 (Reply 3):Thrust lapse often eats up the drag reduction.

I was referring to TAS in my post, since that's what he was asking about - so you don't necessarily need to increase thrust to attain higher TAS as you climb.

 I'm watching Jeopardy. The category is worst Madonna songs. "This one from 1987 is terrible".
 Jetlagged From United Kingdom, joined Jan 2005, 2612 posts, RR: 25 Reply 6, posted Sun Oct 14 2012 14:56:01 UTC (3 years 4 months 1 day 13 hours ago) and read 8367 times:

 Quoting Novice (Thread starter):From the above i take it that the mach number limiting speed is the mach number speed that you reach when you change from IAS to MN?

The words you quoted in the first post refer to limiting speeds and Mach (Vmo, Mmo) not climb speeds and Mach. As Vikkyvik pointed out, climb speeds aren't limiting speeds, but the changeover from using IAS to Mach is similar, though may happen at a different altitude.

In subsonic aircraft, at lower altitudes the limiting factor is dynamic pressure so IAS is the value that is used. The airframe also has a Mach number limit, but at low levels you reach the limiting airspeed first. As you climb the the speed of sound reduces so the Mach number for a given TAS increases. Eventually you get to an altitude where Mmo and Vmo coincide. Above that altitude Mmo becomes the limit.

Climb speed and Mach number are related in a similar way and change over at the altitude where the climb IAS is the same as the climb Mach.

BTW, Mach number is a ratio, not a speed. So you would never say "Mach Number speed".

 The glass isn't half empty, or half full, it's twice as big as it needs to be.
 WingedMigrator From United States of America, joined Oct 2005, 2353 posts, RR: 56 Reply 7, posted Sun Oct 14 2012 21:42:57 UTC (3 years 4 months 1 day 6 hours ago) and read 8291 times:

 Quoting Jetlagged (Reply 6):As you climb the the speed of sound reduces so the Mach number for a given TAS increases.

This is the entire crux of the matter. The speed of sound goes as the square root of temperature, dropping as you climb simply because it gets colder.

 Novice From United Kingdom, joined Aug 2012, 90 posts, RR: 0 Reply 8, posted Tue Oct 16 2012 10:25:27 UTC (3 years 3 months 4 weeks 1 day 18 hours ago) and read 8027 times:

 When climbing at a constant mach number why does the IAS decrease? Is it because the air is less dense i.e less air molecules going through the pitot tube?
 tdscanuck From Canada, joined Jan 2006, 12710 posts, RR: 80 Reply 9, posted Tue Oct 16 2012 11:15:37 UTC (3 years 3 months 4 weeks 1 day 17 hours ago) and read 8015 times:

 Quoting Novice (Reply 8): When climbing at a constant mach number why does the IAS decrease?

Speed of sound is a function of only of temperature (at least in normal air). As you climb, the air is getting colder so the speed of sound is dropping. Thus, to fly at constant Mach, you need to slow down (lower TAS). At the same time, you're climbing so the density is dropping so IAS (even at constant TAS) is also dropping. So you've got a double whammy...your TAS is falling and your IAS is dropping relative to TAS.

Tom.

 Novice From United Kingdom, joined Aug 2012, 90 posts, RR: 0 Reply 10, posted Tue Oct 16 2012 12:51:46 UTC (3 years 3 months 4 weeks 1 day 15 hours ago) and read 7994 times:

 Quoting tdscanuck (Reply 9): Thus, to fly at constant Mach, you need to slow down (lower TAS).

How do you lower your TAS when flying at a constant Mach?

and from jet

 Quoting Jetlagged (Reply 6):In subsonic aircraft, at lower altitudes the limiting factor is dynamic pressure so IAS is the value that is used. The airframe also has a Mach number limit,

Is the mach number limited to do with the adverse affects of flying close to the speed of sound?

 Fabo From Slovakia, joined Aug 2005, 1245 posts, RR: 0 Reply 11, posted Tue Oct 16 2012 13:15:41 UTC (3 years 3 months 4 weeks 1 day 15 hours ago) and read 7983 times:

 Quoting Novice (Reply 10):How do you lower your TAS when flying at a constant Mach?

Physics does it for you. You dont do it yourself, you have a mach indicator and you hold that in place.

 Quoting Novice (Reply 10):Is the mach number limited to do with the adverse affects of flying close to the speed of sound?

You could say that.

 The light at the end of tunnel turn out to be a lighted sing saying NO EXIT
 vikkyvik From United States of America, joined Jul 2003, 11908 posts, RR: 24 Reply 12, posted Tue Oct 16 2012 15:14:36 UTC (3 years 3 months 4 weeks 1 day 13 hours ago) and read 7961 times:

 Quoting Novice (Reply 10):How do you lower your TAS when flying at a constant Mach?

Climb. That's what Tom was talking about. Climb at a constant Mach, and your TAS will decrease.

 I'm watching Jeopardy. The category is worst Madonna songs. "This one from 1987 is terrible".
 georgiaame From United States of America, joined Aug 2005, 1082 posts, RR: 5 Reply 13, posted Tue Oct 16 2012 15:38:30 UTC (3 years 3 months 4 weeks 1 day 12 hours ago) and read 7957 times:

 I love this section, even though as a non engineer and a mathematically challenged individual, I barely have a clue as to what you are talking about. OK, in colloquial English, IAS is indicated air speed. TAS??? Next, my question. All of this stuff is well and good. This past weekend, a total nut job jumped out of a tiny pressurized capsule at 24 miles up trying not to become one with the earth. He went supersonic and lived to tell about it. Not only supersonic, but 839.9MPH for a brief period of time. Can anyone discuss how this topic would apply to this lunatic? In advance, thanks!
 "Trust, but verify!" An old Russian proverb, quoted often by a modern American hero
 vikkyvik From United States of America, joined Jul 2003, 11908 posts, RR: 24 Reply 14, posted Tue Oct 16 2012 15:57:52 UTC (3 years 3 months 4 weeks 1 day 12 hours ago) and read 7952 times:

True AirSpeed. The actual speed of an object through the air.

 Quoting georgiaame (Reply 13):Can anyone discuss how this topic would apply to this lunatic?

Well, he stands a much higher chance of breaking the sound barrier at a higher altitude, since the temperature and therefore the speed of sound are much lower. Also, the air is much thinner, so less drag.

As he descended, his terminal velocity would slow as drag increased, and the speed of sound would increase as temp increases, until he was below the speed of sound.

Now seeing a photo of him with shockwaves emanating from his spacesuit would be awesome!

 I'm watching Jeopardy. The category is worst Madonna songs. "This one from 1987 is terrible".
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