Scholarly record
UNMANNED HELICOPTER TAIL UNIT FEM ANALYSIS
Abstract
This paper is focused on creation of the tail unit FEM strength analysis of the UAV based on helicopter by advanced CAx tools. To perform the analyses were used advanced information technology tools with high precision. For the strength analysis was used solver NASTRAN as a part of software NX. This analysis has shown us, in which locations of the surface design will be the greatest loads during the flights operations and in which points of attachment of the tail unit together with fuselage will be the greatest stress. CAx are able to calculate the maximum deformation of the structure under the effect of load. According to the information that we have collected by numerous repeat calculations, we were able to modify the design to achieve the best possible results. For the sheer size of the problem, it was possible to create another research study to find the best design for our type of unmanned device. Thanks to modern informatics methods, it was possible to create several different types of the UAV tail unit, one of which will be analyzed in the paper.
Publication Impact Profile
- Citations
- Scopus - Citation Indexes: 1
- Captures
- Mendeley - Readers: 3
Publication details
References0
Structured references will appear here after the reference import pass. The count is preserved now so the scholarly record is not incomplete.
Citing literature
Number of times cited according to Crossref: 1
View or Download full articleAccess options
SWS access login
Login as SWS Scientific CommitteeLogin as SWS Scientific PartnerLogin as SWS AuthorAuthors and approved SWS contributors will read and export their own linked papers after identity matching by SWS profile, email and SGEM GlobalID.
For librarian assistance: [email protected]
Purchase Instant Access
- Article can be downloaded after successful payment.
- Article may be used according to SWS library access terms.
- Article cannot be redistributed.