Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell With Several Tail-Fin Configurations Page: 1 of 32
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UNCLASSIFIED
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{CLASSIFICATION CHAN(
RESEARCH MEMORANDUM
for
U. S. Army Ordnance
WIND-TUfNEL INVESTIGATION OF THE EFFECT OF SPIN ON THE AERODYNAMIC
CHARACTERISTICS OF A 60-MILLIMETER T-214 MORTAR SHELL
WITH SEVERAL TAIL-FIN CONFIGURATIONS
By William B. Kemp, Jr., and William C. Hayes, Jr.
Langley Aeronautical Laboratory
CLASS rCATION &'T-gWY Field, Va.
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LANGLE AERONAUTICAL LOArORV
LA , . UBRARY, NACCLASSIFIED DOCUMENT
This material contains information affecting the National Defense of the United States within the meaning
of the espionage laws, Title 18, U.S.C., Sees. 793 and 794, the transmission or revelation of which in any
manner to an unauthorized person is prohibited by law.
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
WASHINGTON
MAR 2 1 1957vYIR UIIA
UNCLASSFIED
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Kemp, William B., Jr. & Hayes, William C., Jr. Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell With Several Tail-Fin Configurations, report, March 21, 1957; (https://digital.library.unt.edu/ark:/67531/metadc63301/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.