Minimum takeoff and landing distances are calculated and various effects considered at various thrust-to-weight ratios; it appears that takeoff to and landing from 50-ft obstacle can be achieved to 400 ft at all-up-weight 60% greater than VTO all-up weight.
Estimation of minimum field requirements of two overloaded, propeller-driven, tilt-wing VTOL aircraft (Including effects of flap setting, runway surface, wind, wing tilt rate and flap boundary layer control)
Canada. Nat Research Council -- Aeronautical Report
1963
41 pages
Report
English
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Engineering Index Backfile | 1957
|Field requirements of overloaded propeller-driven VTOL aircraft
Engineering Index Backfile | 1963
|Tilt-wing propeller VTOL aircraft -- Present status and future role
Engineering Index Backfile | 1959
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