Validity and applicability of static margin parameter defining stability of flexible aircraft is shown to be restricted to conventional aircraft; alternative suggestions for definition of static margin are put forward which can be equally applied to conventional flexible aircraft of past and integrated flexible aircraft of future; calculations carried out on simple slender plate models with linear and nonlinear aerodynamic forces to assess their static stability characteristics. Pt 1-2 indexed in Engineering Index 1961 p 47.
Static aeroelasticity of slender configurations -- 3
Aeronautical Quarterly
Aeronautical Quarterly ; 14 , Part 1
1963
30 pages
Article (Journal)
English
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