Dynamic response and stability of a composite prop-fan model

Cover of: Dynamic response and stability of a composite prop-fan model |

Published by National Aeronautics and Space Administration, Lewis Research Center, For sale by the National Technical Information Service in Cleveland, Ohio, [Springfield, Va .

Written in English

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  • Dynamic response.,
  • Dynamic stability.,
  • Graphite-epoxy composites.,
  • Propeller blades.,
  • Propeller fans.

Edition Notes

Book details

Statementby Arthur F. Smith and Bennett M. Brooks.
SeriesNASA contractor report -- NASA CR-179528.
ContributionsBrooks, Bennett M., Lewis Research Center.
The Physical Object
Pagination1 v.
ID Numbers
Open LibraryOL15411900M

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Dynamic Response and Stability of a Composite Prop-Fan Model CR- 4. Title and Subtitle October, 6. Performing Organization Code 5. Reporl Date 7. [email protected]) * + A. Smith and 8. Brooks 8. Performlng Organization Report No. Perfoming Organization Name and Address Hami 1 ton Standard Division United Technologies Corporation.

Get this from a library. Dynamic response and stability of a composite prop-fan model. [Arthur F Smith; Bennett M Brooks; Lewis Research Center.]. Smith has written: 'Dynamic response and stability of a composite prop-fan model' -- subject(s): Dynamic response, Graphite-epoxy composites, Propeller fans, Propeller blades, Dynamic stability.

Nonlinear Composite Beam Theory Hodges, Dewey H. From an authoritative expert whose work on modern helicopter rotor blade analysis has spanned over three decades, comes the first consistent and rigorous presentation of beam theory.

Results of wind tunnel tests at low forward speed for blade dynamic response and stability of three cm ( in) diameter models of the Prop-Fan, advanced turboprop, are presented. Analytical stability results from this code are compared with published experimental results of a rotating composite advanced turboprop model and of nonrotating metallic wing model.

View Show abstract. Dynamic response and stability of a composite prop-fan model book basic objectives of this contract were to perform detailed analysis and evaluation of dynamic data obtained during Space Shuttle Main Engine (SSME) test and flight operations, including analytical/statistical assessment of component dynamic performance, and to continue the development and implementation of analytical/statistical models to.

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In fact it can be expected, as a consequence of increased opposition to noise by near airport residents. Prop-Fan Engine Turbojets To reach higher (including supersonic) speed is possible by means of turbojet (Fig. It is considered, that specific thrust (the ratio of en- gine thrust to air consumption through it) of turbojet becomes more, and the specific fuel.

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The dynamic response of maglev systems is important in several respects: Safety and ride quality, guideway design, and system costs. The dynamic response of vehicles is the key element in the determination of ride quality, and vehicle stability is one of the important elements.

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