Solution of Rotary-Wing Aeromechanical Problems Using Differential-Algebraic Equation Solvers

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.45, Iss.4, 2000-10, pp. : 253-262

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Review of Rotary-Wing V/STOL Dynamic and Aeroelastic Problems

By Loewy Robert G.

Journal of the American Helicopter Society, Vol. 14, Iss. 3, 1969-07 ,pp. : 3-23

AHS International

Access to resources Recommend Favorite

Rotary-Wing Development

Aircraft Engineering, Vol. 32, Iss. 3, 1993-12 ,pp. : 63-63

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

System Identification of a Rotary-Wing Micro Air Vehicle

By Conroy Joseph K. Humbert J. Sean Pines Darryll J.

Journal of the American Helicopter Society, Vol. 56, Iss. 2, 2011-04 ,pp. : 25001-0

AHS International

Access to resources Recommend Favorite

Application of the Finite Element Method to Rotary-Wing Aeroelasticity

By Friedmann P. P. Straub F.

Journal of the American Helicopter Society, Vol. 25, Iss. 1, 1980-01 ,pp. : 36-44

AHS International

Access to resources Recommend Favorite

History of Air Force Development of Rotary-Wing Aircraft

By Hardy Cyrus W.

Journal of the American Helicopter Society, Vol. 1, Iss. 1, 1956-01 ,pp. : 78-86

AHS International

Access to resources Recommend Favorite