Point drag and total drag of navy struts no. 1 modified

Zahm, A F Smith, R H Hill, G C
naca-report-137
1923


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.

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http://naca.central.cranfield.ac.uk/reports/1923/naca-report-137.pdf