Effects of string-support interference on the drag of an olgive-cylinder body with and without a boatail at 0.6 to 1.4 Mach number Page: 1 of 29
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ffmRESEARCH MEMORANDUM
EFFECTS OF STING-SUPPORT INTERFERENCE ON THE DRAG OF AN
OGIVE-CYLINDER BODY WITH AND WITHOUT A BOATTAIL
AT 0.6 TO 1.4 MACH NUMBER
By George Lee and James L. Summers
Ames Aeronautical Laboratory
Moffett Field, Calif.
AFM2C
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AFL 2811
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
WASHINGTON
December 3, 1957-9. -Z20"P4
NACA
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Lee, George & Summers, James L. Effects of string-support interference on the drag of an olgive-cylinder body with and without a boatail at 0.6 to 1.4 Mach number, report, December 3, 1957; (https://digital.library.unt.edu/ark:/67531/metadc63751/m1/1/: accessed April 17, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.