Range/Temp/Alt-Jets
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Range/Temp/Alt-Jets
Speaking in terms of jet transport and temperature, will a higher temp be more beneficial wrt specific air range?
i.e. if its ISA+50 at 330, won't the benefits of better mach/tas ratio outweigh the -ive of reduced engine efficiency?
i.e. if its ISA+50 at 330, won't the benefits of better mach/tas ratio outweigh the -ive of reduced engine efficiency?
Join Date: Nov 2001
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jtr,
you are right. with higher temp, you get higher TAS but at the same time the air is less dense as a result the engines are less efficient. dont know what is the cut off point, i guess should be ISA+15 or the flat-rated temp.
SR
you are right. with higher temp, you get higher TAS but at the same time the air is less dense as a result the engines are less efficient. dont know what is the cut off point, i guess should be ISA+15 or the flat-rated temp.
SR