Falcon Capt said:
I heard the G-450 was made to feel more like the G-V than the G-IV...
Yep, Gulfstream has been able to shave off 5-8 knots knots (depending on weight) from Vref speeds on the G350/G450 from the old G-IV speeds. Additionally, the G350/G450 benefits from the new FADECs and Auto-Throttles and is flown at Vref +5 rather than Vref + 10 as is done on the G-IV.
Whoever said that the Gulfstream doesn't have leading edge devices because it doesn't need them is exacty correct. The 93.47 ft., 1136.6 sq ft, wide chord, low wing loading wing with a nominal sweep of 27.88 degrees is a Swiss Army knife of a wing design allowing you to do anything from steep turns at 51,000 feet to flying an approach speed of 112 knots without the need of any additional aerodynamic devices.
In the last two weeks I've been into Carlsbad (4800 ft) and Olympia (presently 4600ft) with a Vref no greater than 114 knots and was able to make the mid-field turn-off at both facilities.
Gulfstream's philosophy is that when you buy leading edge devices you pay for them three times. The first when you buy them (complexity adds to costs), the next time to carry them around (weight of actuators and linkage), and the third time to maintain them (complexity adds to required maintenance and failure rate).
From my standpoint, the leading edge on aircraft with slats is nasty. Even with the pristine leading edge on the GV, if we are going out to do stalls we inspect the gap seals to insure that they are not deteriorating. A bad gap seal can inject a stream of high velocity air below the boundary layer on the wing's upper surface and cause early separation and stall.
Thanks for asking.
GV