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Experimental damping-in-pitch of two slender cones at Mach 2 and incidences up to 30 degOscillatory experiments were performed on two slender cones at Mach 2 and incidences up to 30 deg, using three different experimental arrangements. The damping-in-pitch was found to remain constant at incidences of up to a value approximately corresponding to the cone semi-angle, after which an almost linear increase with incidence was noted. The results obtained with the different techniques were in very good agreement up to an incidence of 15 deg and in some cases up to 25 deg.
Document ID
19720021343
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Iyenger, S.
(National Aeronautical Establishment Ottawa Ontario, Canada)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-114483
LTR-UA-19
Report Number: NASA-CR-114483
Report Number: LTR-UA-19
Accession Number
72N28993
Funding Number(s)
CONTRACT_GRANT: NASW-1947
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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