Wind Tunnel Investigation At High Subsonic Speeds Of A Spoiler Slot Deflector Combination On A Naca 65a006 Wing With Quarter Chord Line Swept Back 326
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WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEEDS OF A SPOILER-SLOT- DEFLECTOR COMBINATION ON A NACA 65A006 WING WITH QUARTER-CHORD LINE SWEPT BACK 32.6
Author | : |
Publisher | : |
Total Pages | : 30 |
Release | : 1953 |
Genre | : |
ISBN | : |
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