Number of designs were previously developed around set of common design criteria; these designs used turboprop, fan-in-wing, and propulsive wing propulsion system arrangements; present report summarizes studies of performance of these aircraft when operated at off-design conditions and of design changes resulting from using different design criteria; some of basic aerodynamic input data that were utilized in developing these designs, and noise characteristics of some of designs, were evaluated.
Additional studies on feasibility of V/STOL concepts for short-haul transport aircraft
NASA CR
NASA Contractor Reports ; n 670 (01)
1967
41 pages
Report
English
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