Supersonic wind tunnel testing - scout vehicle fin load and tip control hinge moments
FIN LOADS AND TIP-CONTROL HINGE MOMENTS ON A 1 8-SCALE MODEL SIMULATING THE FIRST STAGE OF THE SCOUT RESEARCH VEHICLE AT A MACH NUMBER OF 2.01
1960-05-01
Report
Keine Angabe
Englisch
NTIS | 1965
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