Dynamic stability calculations were carried out for longitudinal motion of aircraft with delta wing in supersonic region; parameters which are varied in calculations are Mach number, flight altitude, sweep angle, center of gravity location and wing loading; results, obtained partly with digital and analog computer, are analyzed by means of approximated expressions for frequency and damping of components of disturbed motion.
Investigation of dynamic longitudinal stability of delta-winged aircraft at supersonic speeds
Amsterdam. Nationaal Lucht- en Ruimtevaartlaboratorium (Nat Aero- and Astronautical Research Inst) -- Reports and Trans TN
1963
60 pages
Report
English
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