This report deals with the results of tests on struts conducted at Washington Navy Yard. Two models of the modified Navy strut, no. 1, were tested in the 8 by 8 foot wind tunnel. The tests were made to determine the total resistance end effect and the pressure distribution at various wind-tunnel speeds with the length of the strut transverse to the current. Only the measurements made at zero pitch and yaw are given in this report.
Point drag and total drag of navy struts no. 1 modified
1923-01-01
Sonstige
Keine Angabe
Englisch
Interference effects and drag of struts on a monoplane wing
Engineering Index Backfile | 1931
|Hydrodynamic drag of 12- and 21-percent-thick surface-piercing struts
Engineering Index Backfile | 1953
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