drgondog
Major
CL is lower for same speed at lower altitudes. It is inversely proportional to air density when holding V the same.
Parasite drag due to lift is non-linear and really shows up at higher altitudes when you have to fly a higher AoA (and CL) to get the same lift. Recall the conundrum of the U-2 stall speed nearly the same as max speed at extreme altitudes. Cranking up AoA to stay in the air until nearly reach a CL stall break
So, lower altitudes drives lower CL = lower Induced Drag. True, the Parasite drag due to profile drag of the wing and fuselage also reduces with increased altitude but at optimal cruise speed for a given altitude, the Parasite Drag=Induced Drag
And last but not least, the engine isn't working as hard to produce thrust -----> lower fuel consumption to get the optimal speeds for long range cruise.
Parasite drag due to lift is non-linear and really shows up at higher altitudes when you have to fly a higher AoA (and CL) to get the same lift. Recall the conundrum of the U-2 stall speed nearly the same as max speed at extreme altitudes. Cranking up AoA to stay in the air until nearly reach a CL stall break
So, lower altitudes drives lower CL = lower Induced Drag. True, the Parasite drag due to profile drag of the wing and fuselage also reduces with increased altitude but at optimal cruise speed for a given altitude, the Parasite Drag=Induced Drag
And last but not least, the engine isn't working as hard to produce thrust -----> lower fuel consumption to get the optimal speeds for long range cruise.