View Full Version : Tas Vs Lss ??
theaviator2005
24th May 2010, 09:03
Hi, just have a few questions that im discussing with a few guy's.
Were talking about TAS vs LSS (local speed of sound)
We do know that LSS is dependent on Temperature so with a decrease in temp we get a decrease in LSS. BUT!!!
How do they work agains each other TAS and LSS.
If one increases what happens to the other and vise verse!!!
hetfield
24th May 2010, 09:09
Scroll a bit further down in this forum....
latetonite
24th May 2010, 09:10
TAS has no direct relationschip to LSS.
theaviator2005
24th May 2010, 09:25
Ya thats what i was saying aswell that TAS does not have any direct relationship to LSS, but were discussing a question that was given at a Airline interview where it was asked: What happens to LSS or TAS if one increases or the other decreases?
Didnt make much sense to me as i do not believe that they are directly related.
Anyways
Thanks
;-)
FLEXPWR
24th May 2010, 10:21
If it is the relationship to the Mach number you're looking for, then there is a simple way to remember, here we go:
Chicken Tikka Massala :}
C for Calibrated (most aircraft today display CAS as IAS)
T for True airspeed (TAS)
M for Mach
At sea level, in ISA, all 3 should nearly be in the same spot, as well as Ground Speed if there is no wind.
As you gain altitude, C is less than T, and T is less than M.
3 possible scenarios (scenarii for the purists):
Constant CAS = TAS & Mach will increase with altitude
Constant TAS = CAS decreases and Mach increases with altitude
Constant Mach = CAS & TAS decrease with altitude
But I am probably off-topic, unless your question was about the Mach, and not the LSS.
Flex
Poose
24th May 2010, 13:03
Have a gander at the Local Speed of Sound thread. There's some good explanations on there. :ok: