Accession Number:

AD0612415

Title:

EXPERIMENTAL RESEARCH OF NATURAL OSCILLATIONS OF A SQUARE PLATE IN A SUPERSONIC FLOW,

Personal Author(s):

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1965-03-09

Abstract:

Investigation is made of the natural oscillations flutter of a flat square plate in a supersonic flow at Mach 1.7, 2.3, and 3 for the case where two edges of the plate are perpendicular to the flow and fastened and two edges parallel to the flow are open. The results of the experiment are compared with a theoretical solution. Author

Supplementary Note:

Unedited rough draft trans. of Akademiya Nauk SSSR. Izvestiya. Mekhanika i Mashinostroenie, 1959, no. 1, p. 154-157.

Pages:

0011

Descriptors:

File Size:

0.00MB

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