Results of combined flight and ground-based dynamic flight simulator study of handling and riding qualities problems associated with low altitude, high speed flight; wide variations of longitudinal stability and control characteristics, considered representative of current and future strike aircraft, were pilot evaluated; results are presented in terms of iso-opinion and iso-performance boundaries defining desired and required stability and control parameters for low altitude, high speed flight; these acceptance boundaries are significantly different from boundaries defined in Military Specifications. (See also J of Aircraft v 1 n 1 Jan-Feb 1964 p 32-40)
Low-altitude, high-speed handling and riding qualities
AGARD -- Report
1963
44 pages
Report
English
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Low-altitude, high-speed handling and riding qualities
AIAA | 1964
|Low-altitude, high-speed handling and riding qualities
AIAA | 1963
|Low-altitude, high-speed handling and riding qualities
Engineering Index Backfile | 1964
|