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Flight flutter testing using pulse techniquesA case of flutter developed at a speed lower than had been flown previously. This incident precipitated the routine procedure of pulsing control surfaces as well as the firing of explosive charges during speed build-ups. In the interest of rapid evaluation of results, simple methods of data reduction were used. A case history is presented where in the pulse technique predicted flutter by extrapolating decay rates obtained at subcritical speeds; in addition, a case is presented where no valid extrapolation could be made.
Document ID
19760003016
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stringham, R. H., Jr.
(Douglas Aircraft Co., Inc. El Segundo, CA, United States)
Lenk, E. J.
(Douglas Aircraft Co., Inc. El Segundo, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA, Washington Flight Flutter Testing Symp.
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N10104
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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