The article presents the results of an experimental study of the damping moment coefficients of the configuration of supersonic airliner models with small wing aspect ratios in a supersonic wind tunnel. A comparison of experimental and calculated data is presented.
A Study of the Damping Characteristics on Models of Supersonic Airlines at Supersonic Speeds
1974
11 pages
Report
Keine Angabe
Englisch
Online Contents | 1994
Online Contents | 1994
Online Contents | 1994
Online Contents | 1994
Engineering Index Backfile | 1949
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