Static Aerodynamic Characteristics Of A Scout Fin With An Enlarged Tip Control At Mach Numbers From 040 To 463
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Static Aerodynamic Characteristics of a Scout Fin with an Enlarged Tip Control at Mach Numbers from 0.40 to 4.63
Author | : Robert J. Keynton |
Publisher | : |
Total Pages | : 60 |
Release | : 1971 |
Genre | : Aircraft |
ISBN | : |
Download Static Aerodynamic Characteristics of a Scout Fin with an Enlarged Tip Control at Mach Numbers from 0.40 to 4.63 Book in PDF, Epub and Kindle
Results are presented of an experimental investigation to determine the static longitudinal aerodynamic characteristics of a fin with an enlarged tip control and the hinge-moment coefficients of the enlarged tip control. The model was tested at angles of attack from -6 [degree] to 6 [degree] and fin tip control deflections from -20° to 20°. A 1/8-scale model of the Scout first stage, with a tangent ogive nose, was used for these tests. Basic data obtained include the pitching-moment, rolling-moment, and normal-force coefficients of the fin and the hinge-moment coefficient of the enlarged tip control.
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