Aerodynamic characteristics in pitch of variable sweep V/STOL configurations tested in supersonic wind tunnel
Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75 deg
1960-10-01
Report
Keine Angabe
Englisch
Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations
Online Contents | 2013
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