Idioma:

T-splines computational membrane–cable structural mechanics with continuity and smoothness: II. Spacecraft parachutes

Terahara, Takuya ; Takizawa, Kenji ; Avsar, Reha ; Tezduyar, Tayfun E.

Computational mechanics, 2023-04, Vol.71 (4), p.677-686 [Periódico revisado por pares]

Berlin/Heidelberg: Springer Berlin Heidelberg

Texto completo disponível

Citações Citado por

Enviar para

Título:
T-splines computational membrane–cable structural mechanics with continuity and smoothness: II. Spacecraft parachutes
Autor: Terahara, Takuya ; Takizawa, Kenji ; Avsar, Reha ; Tezduyar, Tayfun E.
Assuntos: Analysis ; Basis functions ; Classical and Continuum Physics ; Computational Science and Engineering ; Engineering ; Mathematical models ; Mechanics ; Mechanics (physics) ; Membranes ; Original Paper ; Parachute canopies ; Smoothness ; Space ships ; Space vehicles ; Spacecraft ; Spline functions ; Theoretical and Applied Mechanics ; Wind tunnels
É parte de: Computational mechanics, 2023-04, Vol.71 (4), p.677-686
Descrição: In this second part of a two-part article, we present spacecraft parachute structural mechanics computations with the T-splines computational method introduced in the first part. The method and its implementation, which was also given in the first part, are for computations where structures with different parametric dimensions are connected with continuity and smoothness. The basis functions of the method were derived in the context of connecting structures with 2D and 1D parametric dimensions. In the first part, the 2D structure was referred to as “membrane” and the 1D structure as “cable.” The method and its implementation, however, are certainly applicable also to other 2D–1D cases, and the test computations presented in the first part included shell–cable structures. Similarly, the spacecraft parachute computations presented here are with both the membrane and shell models of the parachute canopy fabric. The computer model used in the computations is for a subscale, wind-tunnel version of the Disk–Gap–Band parachute. The computations demonstrate the effectiveness of the method in 2D–1D structural mechanics computation of spacecraft parachutes.
Editor: Berlin/Heidelberg: Springer Berlin Heidelberg
Idioma: Inglês

Voltar para lista de resultados

Anterior Resultado 10 Avançar Ir para próxima página

Realização: Logos de Redes Sociais:

T-splines computational membrane–cable structural mechanics with continuity and smoothness: II. Spacecraft parachutes

Terahara, Takuya ; Takizawa, Kenji ; Avsar, Reha ; Tezduyar, Tayfun E.

Berlin/Heidelberg: Springer Berlin Heidelberg

Buscando em bases de dados remotas. Favor aguardar.