ahurst
Getting familiar with the group...
I am a bit anal when researching for a car purchase.
I like to figure power-to-weight ratios using HP/weight.
The tweak this time for me is I am living in Colorado at 6,500 feet. Most drivers here buy turbocharged engines to compensate for engine power loss above sea level.
Turbo engines also lose power at high altitude but to a much lesser degree than NA engines.
The chart below lists the power-to-weight ratios for cars I am looking at -- some with NA engines and some turbocharged.
The Genesis 4.6 surprisingly finished highest.
HP @ 6,000 ft--Model--------Weight--HP/Weight
316------------Genesis 4.6---4012----0.0787
296------------Audi S4-------3924----0.0755
325------------Taurus SHO---4368----0.0744
269------------Infiniti G37----3615----0.0744
263------------335i----------3593----0.0731
263------------335xi---------3814----0.0688
316------------Ford Flex-----4839----0.0653
238------------Genesis 3.8---3748----0.0634
The formula I used for NA engines was 6,000ft * .03 * HP / 1000.
The formula for turbo engines was max boost at 6,000 ft / max boost at sea level. This ratio was applied to the sea level HP of the engine to come up with HP at altitude.
For example, even though the SHO is rated at 365 HP - at 6,000 feet it will only put out 325. The Genesis drops to 316. But because of the 300 pound weight difference, the Genesis has a better power-to-weight ratio.
Does this sound right?
I like to figure power-to-weight ratios using HP/weight.
The tweak this time for me is I am living in Colorado at 6,500 feet. Most drivers here buy turbocharged engines to compensate for engine power loss above sea level.
Turbo engines also lose power at high altitude but to a much lesser degree than NA engines.
The chart below lists the power-to-weight ratios for cars I am looking at -- some with NA engines and some turbocharged.
The Genesis 4.6 surprisingly finished highest.
HP @ 6,000 ft--Model--------Weight--HP/Weight
316------------Genesis 4.6---4012----0.0787
296------------Audi S4-------3924----0.0755
325------------Taurus SHO---4368----0.0744
269------------Infiniti G37----3615----0.0744
263------------335i----------3593----0.0731
263------------335xi---------3814----0.0688
316------------Ford Flex-----4839----0.0653
238------------Genesis 3.8---3748----0.0634
The formula I used for NA engines was 6,000ft * .03 * HP / 1000.
The formula for turbo engines was max boost at 6,000 ft / max boost at sea level. This ratio was applied to the sea level HP of the engine to come up with HP at altitude.
For example, even though the SHO is rated at 365 HP - at 6,000 feet it will only put out 325. The Genesis drops to 316. But because of the 300 pound weight difference, the Genesis has a better power-to-weight ratio.
Does this sound right?