Stability And Drag Characteristics At Mach Numbers From 08 To 15 Of A Free Flight Model Having 3 Percent Thick 60 Degree Triangular Wing And Horizontal Tail Surfaces
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Stability and Drag Characteristics at Mach Numbers from 0.8 to 1.5 of a Free-flight Model Having 3-percent-thick, 60 Degree Triangular Wing and Horizontal Tail Surfaces
| Author | : Rowe Chapman |
| Publisher | : |
| Total Pages | : 30 |
| Release | : 1954 |
| Genre | : Airplanes |
| ISBN | : |
Download Stability and Drag Characteristics at Mach Numbers from 0.8 to 1.5 of a Free-flight Model Having 3-percent-thick, 60 Degree Triangular Wing and Horizontal Tail Surfaces Book in PDF, Epub and Kindle
A flight test of a rocket-propelled model having 60 degree triangular wing and horizontal tail surfaces 3 percent thick was made to investigate the stability and drag of the configuration. Drag and stability data are compared with similar triangular-wing configurations.
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