Reduction in Flutter Instability of an Elastic Beam with the Rigid Empennage in Supersonic Flow,

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Abstract:

The possibility of the expansion of the region of dynamic elastic stability of a finned beam streamlined by a supersonic gas flow is investigated. In order to do this a system of automatic control, which consists of the object of control, measuring elements and actuators, is used.

Author(s):
Selezov, I. T. ; Kovbasa, G. T.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited machine trans. of Gidroaeromekhanika i Teoriya Uprugosti (USSR) n9 p29-34 1970, by Robert D. Hill.
Annotation:
Reduction in Flutter Instability of an Elastic Beam with the Rigid Empennage in Supersonic Flow--Translation.
Pagination:
0014

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-MT-24-97-71
Project Number(s):
FTD-137003030
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
(*TAILS(AIRCRAFT), FLUTTER), SUPERSONIC CHARACTERISTICS, STABILITY, ELASTIC PROPERTIES, AUTOMATIC, USSR
Field(s)/Group(s):
Aerodynamics, Aircraft, Fluid Mechanics
Keyword(s):
TRANSLATIONS
Report Date:
1971 Nov 18