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Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations

Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations - - Washington, D.C. National Aeronautics & Space Administration 1978 - 76 p. - NASA TP 1291 : 1978 .

ISBN:

Subjects--Topical Terms:

Aerodynamic damping, Dynamic stability, Canard

Universal Decimal Class. No.: LNASA TP 1291 : 1978

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