Aeroelastic Trim Analysis of Very Flexible Aircraft Based on 3-D Lifting-Line Theory
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
01.01.2013
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aeroelastic Trim Analysis of Very Flexible Aircraft Based on 3-D Lifting-Line Theory
British Library Conference Proceedings | 2013
|NONLINEAR STATIC AEROELASTIC AND TRIM ANALYSIS OF HIGHLY FLEXIBLE AIRCRAFT
British Library Conference Proceedings | 2018
|Static Aeroelastic Analysis of Very Flexible Wing Based on the 3-D Lifting-Line Theory
British Library Conference Proceedings | 2012
|