NASA NACA-TN-1743-1948 Flight measurements of the stability control and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-data.pdf
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NASA NACA-TN-1743-1948 Flight measurements of the stability control and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-data.pdf
1、.?LIGHTv/NATIONAL ADVISORY COMMITTEEFOR AERONAUTICSTECHNICAL NOTENo. 1743MEASUREMENTSOF THE STA, CONTROL, AND STALLINGCHARACTERISTICS OF AN AIRPLANE HAVING A 35 SWEPTEACK VLINGWITHOUT SLOTS AND WITH 80 -PERCENT-SPAN SLOTS AND AComparison WTTH WIND-TUNNEL DATABy S. A. Sjoberg and J. P. ReederLangley
2、Aeronautical LaboratoryLangley Field, Va.WashingtonNovember 1948- - -., .-., , :,” ,“/4,- +.- - . . . . . . . . . . . . . - -. . .4,-,.I-JProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-) C Qfgh?(b) Vc = 125ties perhour;CN = O.W.Figure9.- Continued.-c -. - . .-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
