AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS
Author | : Bernard Spencer |
Publisher | : |
Total Pages | : 32 |
Release | : 1960 |
ISBN-10 | : NASA:31769000459803 |
ISBN-13 | : |
Rating | : 4/5 ( Downloads) |
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