Parametric flutter studies of an arrow-wing configuration : Some early results

Author:: Parker, Ellen C.
Published:: May 1, 1988.
Physical Description:: 1 electronic document
Additional Creators:: Keller, Donald F., Wilkie, W. Keats, Cazier, F. W., Jr., Cole, Stanley R., and Durham, Michael H.

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Summary:

Some early experimental results from a combined experimental and analytical study being conducted at NASA-Langley of the transonic flutter characterisitics of a generic arrow wing configuration are presented. The planned study includes the parametric variation of a variety of structural and geometric characteristics. Presented here are flutter results of the basic arrow wing, for the basic wing with the addition of two simulated lower-surface-mounted engine nacelles, and for the basic wing with the addition of both the fin and the engine nacelles.

Other Subject(s):

AERODYNAMICS

Collection:

NASA Technical Reports Server (NTRS) Collection.

Note:

Document ID: 19880016060.
Accession ID: 88N25444.
NASA-TM-100608.
NAS 1.15:100608.

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