Zero-Lift Drag of 60° Delta-Wing -- Body Combination (AGARD Model 2) Obtained from Free-Flight Tests Between Mach Numbers of 0.8 and 1.7.
Zero-lift Drag of 60° Delta-wing -- Body combination (AGARD Model 2) obtained from free-flight tests between mach numbers of 0.8 and 1.7
NACA -- Tech Note
1954
11 pages
Report
Englisch
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