The article talks about 800fpm in relation to Vortex Ring State, not max rate of descent for landing. I know for a Shitter, at least, if you landed at 800fpm, you could log multiple landings and the struts would be through your sponsons. (if we're light 672fpm is our max rod landing)
Let me preface this with, I am not an aerodynamics nerd or test pilot, but >800fpm rod and less than 40kts is what everyone is taught as parameters for Vortex Ring State. These numbers are pretty generic. The gouge I've heard is that the airspeed for VRS is 40kts b/c of unreliability of pitot static system below 40kts, and the 800fpm rod comes from tests done with Hueys a long time ago. I know for a fact that a 53 will not enter VRS at even close to these parameters, and I suspect the Osprey would not either.
The author makes a lot of assertions that don't quite add up. It sounds like there is definitely an agenda behind the article...
Let me preface this with, I am not an aerodynamics nerd or test pilot, but >800fpm rod and less than 40kts is what everyone is taught as parameters for Vortex Ring State. These numbers are pretty generic. The gouge I've heard is that the airspeed for VRS is 40kts b/c of unreliability of pitot static system below 40kts, and the 800fpm rod comes from tests done with Hueys a long time ago. I know for a fact that a 53 will not enter VRS at even close to these parameters, and I suspect the Osprey would not either.
The author makes a lot of assertions that don't quite add up. It sounds like there is definitely an agenda behind the article...