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Accession Number:
AD0857892
Title:
Dynamic Tests of a 10-Deg Cone Having Three Angular Degrees of Freedom at Mach 8
Corporate Author:
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
Report Date:
1969-09-01
Abstract:
Dynamic stability data were obtained on a slightly blunted 10-deg half-angle cone at Mach number 8. The tests were conducted using a unique balance system which allowed the model to have three angular degrees of freedom. Both a symmetrical model and a model having compound configurational asymmetries were tested at free-stream Reynolds numbers, based on model length, of from 1, 610,000 to 2,950,000. Data obtained on the symmetrical model at roll rated up to 300 revmin showed the damping-in-pitch derivatives to be nearly constant with roll rate.
Descriptive Note:
Final rept.
Supplementary Note:
Prepared in cooperation with ARO, Inc., Tullahoma, Tenn.
Pages:
0028
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
F40600-69-C-0001
File Size:
1.16MB
