An Approximation to the Influence Function for Plate-like Wings: A General Solution for Small Deflexions

By D.C.Ae. R.D. Milne   B.Sc.  

Aircraft Engineering, Vol. 31, Iss. 6, 1993-12 ,pp. : 156-162

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Identification of Helicopter Dynamics Using Recurrent Neural Networks and Flight Data

By Kumar M. Vijaya   Omkar S. N.   Ganguli Ranjan   Sampath Prasad   Suresh S.  

Journal of the American Helicopter Society, Vol. 51, Iss. 2, 2006-04 ,pp. : 164-174

AHS International

Access to resources Recommend Favorite

Automatic Identification of Modal Damping from Floquet Analysis

By Nagabhushanam J.   Gaonkar G. H.  

Journal of the American Helicopter Society, Vol. 40, Iss. 2, 1995-04 ,pp. : 39-42

AHS International

Access to resources Recommend Favorite

Aircraft flutter prediction using experimental modal parameters

By Pankaj Achuthan C.   Shanthini G.   Shivaprasad M.V.   Manjuprasad M.  

Aircraft Engineering, Vol. 85, Iss. 2, 2013-03 ,pp. : 87-96

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

A General Method for Modifying a Finite-Element Model to Correlate with Modal Test Data

By Twomey William J.   Chen Timothy L. C.   Ojalvo Irving U.   Ting Tienko  

Journal of the American Helicopter Society, Vol. 36, Iss. 3, 1991-07 ,pp. : 48-58

AHS International

Access to resources Recommend Favorite