Wind Tunnel Investigation At High Subsonic Speeds Of The Effect Of Spoiler Profile On The Lateral Control Characteristics Of A Wing Fuselage Combination Winter Quarter Chord Line Swept Back 326c And Naca 65a006 Airfoil Section
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Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination with Quarter-chord Line Swept Back 32.6 Degrees and NACA 65A006 Airfoil Section
| Author | : Harold S. Johnson |
| Publisher | : |
| Total Pages | : 15 |
| Release | : 1953 |
| Genre | : |
| ISBN | : |
Download Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination with Quarter-chord Line Swept Back 32.6 Degrees and NACA 65A006 Airfoil Section Book in PDF, Epub and Kindle
