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 |
| ISBN-10 | : OCLC:1109520772 |
| ISBN-13 | : |
| Rating | : 4/5 ( Downloads) |
Book Synopsis 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 by : Harold S. Johnson
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