Flight Investigation from High Subsonic to Supersonic Speeds to Determine the Zero-lift Drag of a Transonic Research Vehicle Having Wings of 45 Degree Sweepback, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Sections
27.10.1949
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1956
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