Computational, unsteady transonic aerodynamics and aeroelasticity about airfoils and wings [PDF]
Research in the area of computational, unsteady transonic flows about airfoils and wings, including aeroelastic effects is reviewed. In the last decade, there have been extensive developments in computational methods in response to the need for computer ...
Goorjian, Peter M., Guruswamy, Guru P.
core +1 more source
Loads and aeroelasticity division research and technology accomplishments for FY 1985 and plans for FY 1986 [PDF]
The Langley Research Center Loads and Aeroelasticity Division's research accomplishments for FY85 and research plans for FY86 are presented. The rk under each branch (technical area) will be described in terms of highlights of accomplishments during the ...
Dixon, S. C., Gardner, J. E.
core +1 more source
THE DISCRETE VORTEXES METHOD WITH THE IMPROVED QUADRATURE FORMULAE IN THE AEROELASTICITY PROBLEMS
Научный вестник МГТУ ГА, 2016 The possibility of the improved quadrature formulae of the discrete vortexes method used in the aeroelasticity problems is considered. Some of the calculation results confirm the efficiency of these formulae are carried out.
V. V. Ovchinnicov +2 more
doaj
An analytical study of effects on aeroelasticity on control effectiveness [PDF]
Various uses of the Elastic Stability Derivative (ELASRAD) program are described. Topics include structural influence coefficient matrices of wings, arrow wing structural analysis, and graphic display of wing structures.
Mehrotra, S. C.
core +1 more source
Multiparameter spectral analysis for aeroelastic instability problems
, 2017 This paper presents a novel application of multiparameter spectral theory to the study of structural stability, with particular emphasis on aeroelastic flutter.
Gutschmidt, Stefanie, Pons, Arion
core +1 more source
Simulation of flow around oscillating rotor blade section with aeroelastic flap [PDF]
, 2015 Flows around rotor blade sections equipped with active flaps with a degree of freedom in the flap deflection angle are considered in this paper. Results for oscillating flaps are presented.
Barakos, G.N. +5 more
core +1 more source
Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm [PDF]
, 2022 Peng Jin, Qihao Zheng, Wei Wei
openalex +1 more source
THE COMPLEX OF STANDS FOR TESTING THE AIR CUSHION CHASSIS OF AIRCRAFT AND VEHICLES
Научный вестник МГТУ ГА, 2016 This article deals with a set of stands made in NIMK TSAGI for testing and creating the air cushion chassis for the aircraft and vehicles. It allows to fully embrace the process of developing and constructing the air cushion chassis for aircraft and ...
V. A. Brusov +3 more
doaj
Unsteady Lifting-Line Free-Wake Aerodynamic Modeling for Morphing Wings
AerospaceA time-stepping, lifting-line solution algorithm for the prediction of the unsteady aerodynamics of morphing wings is presented. The velocity induced by the wake vorticity is determined through a free-wake vortex-lattice model, whereas the Küssner and ...
Gregorio Frassoldati +3 more
doaj +1 more source