This article proposes a method for investigation of the velocity field behind a low-flying wing with fuselage. The value of the velocity field is necessary in calculating the aerodynamic characteristics of the tail assembly of aircraft which use the screen effect.
Investigation of Velocity Field Behind Low-Flying Wing with Fuselage
1977
21 pages
Report
Keine Angabe
Englisch
Lightweight fuselage for flapping-wing flying robot and flapping-wing flying robot
Europäisches Patentamt | 2022
|Engineering Index Backfile | 1938
|Engineering Index Backfile | 1938
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