Limited test program is being conducted on prototype of Canadair CL-84 tilt-wing V/STOL aircraft to evaluate its stability and control design objectives; results indicate that only very minor modifications were necessary with regard to flying control criteria previously established through analysis, fixed-base simulator studies, and variable-stability helicopter tests; qualitative assessment made thus far of handling qualities of CL-84 has proven adequacy of established criteria for stability and control performance for systems as complex as that of CL-84.
Report on stability and control testing of tilt wing V/STOL aircraft
SAE -- Paper
SAE Meeting ; 1966
1966
15 pages
Conference paper
English
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A Report on Stability and Control Testing of a Tilt Wing V/STOL Aircraft
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