No. First off, too much weight for the truck.Is this real?
Been a long time since I weighed one, but just rough numbers for an empty weigh on a -200 Adv... we'd see about 40,000lbs on each main and about 15-20k on the nose. Add in the stuff to operate and the down force on the nose from deceleration and we're lookin' at 10 to 15 tons that truck needs to support.Is this real?
I rhought airplanes were "lighter than than air"!!!Been a long time since I weighed one, but just rough numbers for an empty weigh on a -200 Adv... we'd see about 40,000lbs on each main and about 15-20k on the nose. Add in the stuff to operate and the down force on the nose from deceleration and we're lookin' at 10 to 15 tons that truck needs to support.
Lift is made up of three components.I have done the math. Long ago. A Lear has ~ 2 4x8 sheets of plywood for each main wing (gross generalization) . 128 sq feet with a 8 degree AOA develops plenty of lift for a loaded Lear at 130 kts absent any foil design/naca numbers. The foil helps dealind well with various surface velocities bur it seems AOA does the actual lifting. Food for thought. I have spent a good part of my life watching, studieing, adjusting foil shapes on sail boats and sailboards.
The "Golden Age of Travel"? My first flights, aged 12, Milwaukee to New York to Dublin and back were, I assume, 707s. I never had a fascination with lesser birds except maybe the venerable DC3. I do remember wearing our "Sunday Best" boarding the aircraft (on a roll up stairway on the apron)
We called 'em Shithooksthe RAF's Chinooks known locally as Wocka-Wockas.