Examination of high speed aeroelastic effects on maneuver point, with special reference to effect of rearward movement of local aerodynamic centers at supercritical Mach numbers; it is concluded that as regards possible shifts of maneuver point, aeroisoclinic wing is generally superior to conventional wing; for tailless aircraft, application of aeroisoclinic principle makes it possible to employ wings of aspect ratio much larger than practicable with conventional design.
Manoeuvre point properties of aero-isoclinic wing
Aircraft Eng
Aircraft Engineering ; 24 , n 283
1952
6 pages
Article (Journal)
English
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