AIAA-2002-4511 Prediction of the Nonlinear Aerodynamic Characteristics of Tandem-Control and Rolling-Tail Missiles
Conference, Atmospheric flight mechanics ; 2002 ; Monterey, CA
01.01.2002
11 pages
Contains paper nos AIAA-2002-4400 to AIAA-2002-5048 with gaps
Aufsatz (Konferenz)
Englisch
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