ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCES
In realizing a high-performance composite material, it is important to take into consideration all the factors that influence the structural response of the component when exposed to service conditions. Thus, in the case of the laminar skin of a composite tail rotor blade, the study of the stress...
Main Authors: | Andrei - Daniel VOICU, Anton HADĂR, Daniel VLĂSCEANU |
---|---|
Format: | Article |
Language: | English |
Published: |
Editura Academiei Oamenilor de Știință din România
2020-08-01
|
Series: | Annals: Series on engineering sciences (Academy of Romanian Scientists) |
Subjects: | |
Online Access: | http://aos.ro/wp-content/anale/TVol12Nr1Art.8.pdf |
Similar Items
-
Response, Loads And Stabillity Of Helicopters With Interconnected Rotor Blades
by: Suresh, J K
Published: (2012) -
Inverse methodology for multi-point aerodynamic rotor blade design
by: Tapia, Fidencio
Published: (2007) -
A numerical solution of implicit nonlinear equations of motion for rotor blades
by: Kim, Young K.
Published: (2006) -
Study of an asymptotic method for helicopter rotor blade aerodynamic loads
by: Vaidyanathan, Anand Ramabhadran
Published: (2006) -
COMPUTATIONAL STUDY OF AERODYNAMIC CHARACTERISTICS OF SINGLE-ROTOR HELICOPTER TAIL ROTOR UNDER THE INFLUENCE OF VORTICAL WAKE OF MAIN ROTOR AT THE HOVER WITH CROSSWIND
by: Yu. M. Ignatkin, et al.
Published: (2017-01-01)