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Sensitivity analysis on the CUSUM method

✍ Scribed by R. Radharamanan; A. Galelli; D.T. Alex; L.L. Perez


Publisher
Elsevier Science
Year
1994
Tongue
English
Weight
603 KB
Volume
33
Category
Article
ISSN
0925-5273

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A novel method has been developed for calculating gradients of aerodynamic force and moment coe$cients for an aeroelastic aircraft model. This method is intended for use in preliminary-level aircraft design which typically involves computationally expensive aerodynamic and structural analyses. This