The volume presents the results of a low speed wind tunnel test of four half-span wing models. The primary objective of the test was to obtain experimental data on wings developed by a high lift surface computer program. Two wings designed by this method, one high and one low lift, were tested. A secondary objective of the test was to determine the feasibility of simulating the high lift wing by flaps on the low lift wing and, conversely, simulating the low lift wing by flaps on the high lift wing. This involved an additional two models for a total of four. (Author)
High Lift Surface; Design Procedures; Experimental Verification. Volume III. Wind Tunnel Tests
1966
2 pages
Report
Keine Angabe
Englisch
Aircraft , Wings , Lift , Design , Model tests , Wind tunnels , Programming(Computers) , Surfaces
Wind-tunnel tests on the experimental high lift M.18
TIBKAT | 1951
|Wind-tunnel tests of hall high-lift wing
Engineering Index Backfile | 1932
|Wind tunnel tests of a hall high lift wing
SLUB | 1932
|Advanced Design by Numerical Methods and Wind-Tunnel Verification Within European High-Lift Program
Online Contents | 2009
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