Wind Tunnel Investigation At High Subsonic Speeds To Determine The Rolling Derivatives Of Two Wing Fuselage Combinations Having Triangular Winds Including A Semiempirical Method Of Estimating The Rolling Derivatives
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Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives
Author | : James W. Wiggins |
Publisher | : |
Total Pages | : 36 |
Release | : 1954 |
Genre | : Airplanes |
ISBN | : |
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