B737 Glide Performance
Joined: Jan 2006
Posts: 2,205
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From: US
Originally Posted by hawk37
Misd-Agin. thanks for the info. Sound like the fmc data is true minimum drag speed, in which case holding at said speed seems likely quite a handful.
Do the fmc holding speeds (I presume they are in KIAS) increase with altitude? This would make sense as minimum drag KCAS is also expected to increase with altitude.
Hawk
Do the fmc holding speeds (I presume they are in KIAS) increase with altitude? This would make sense as minimum drag KCAS is also expected to increase with altitude.
Hawk

Joined: May 2003
Posts: 412
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Based on some generic numbers, you can make an estimate. Lets confine our thoughts to low altitude (ie less compressibility), and a rough figure of 6 % better specific range at max range speed (you should be able to get an exact figure from the performance sections for the aircraft with and without winglets). Assume a flat thrust curve vs velocity.
You've now got approx 6 % less total drag, even though the winglets add parasite drag, and the added weight gives added induced drag. However that is at max range speed about 1.3 times min drag speed. So at min drag speed, expect about 5% less drag (induced drag will be higher at the slower speed, but the reduction of parasite drag will be even more since it increases with TAS squared).
So, expect a 5 % increase in glide distance. It it was 20:1, expect about 21:1
You've now got approx 6 % less total drag, even though the winglets add parasite drag, and the added weight gives added induced drag. However that is at max range speed about 1.3 times min drag speed. So at min drag speed, expect about 5% less drag (induced drag will be higher at the slower speed, but the reduction of parasite drag will be even more since it increases with TAS squared).
So, expect a 5 % increase in glide distance. It it was 20:1, expect about 21:1




