This note presents the results of flight pressure distribution tests on the right upper wing panel of a Douglas M-3 airplane equipped with a semicircular wing tip. The results are given in tables and curves in such form that the load distribution for any force coefficient within the usual range encountered in flight may easily be determined.
The pressure distribution over a semicircular wing tip on an airplane in flight
1931-05-01
Sonstige
Keine Angabe
Englisch
Pressure distribution over semicircular wing tip on biplane in flight
Engineering Index Backfile | 1931
|Pressure distribution over a wing and tail rib of a VE-7 and of a TS airplane in flight
Engineering Index Backfile | 1927
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