Application of time-linearized methods to oscillating wings in transonic flow and flutter

Title

Application of time-linearized methods to oscillating wings in transonic flow and flutter

 Author

Hounjet, M.H.L.
Meijer, J.J.

Institution

National Aerospace Laboratory NLR

 Date

1984-08-15

 Abstract

Unsteady aerodynamic loads in the transonic domain have been obtained with time-linearized methods in which a so-called field panel method is embedded which accounts for a proper radiation of signals towards infinity. The methods are used to predict the unsteady loads and first harmonic pressure distributions on an airfoil and a transport type wing. Results obtained with these methods have been correlated with data of unsteady experiments and also with results of other calculation methods. Transonic flutter applications have been made to a fighter-type configuration.

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http://resolver.tudelft.nl/uuid:0c700e7a-13c9-4056-8c9f-e06b2230ba65

 Publisher

Nationaal Lucht- en Ruimtevaartlaboratorium

 Access restriction

Campus only

 Source

NLR MP 84077 U

 Part of collection

Aerospace Engineering Reports

 Document type

report

 Rights

(c)1984 National Aerospace Laboratory NLR
Files
PDF 84077.pdf 14.17 MB
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