Zobrazeno 1 - 10
of 223
pro vyhledávání: '"Philip S. Beran"'
Publikováno v:
Algorithms, Vol 15, Iss 4, p 131 (2022)
The simultaneous optimization of aircraft shape and internal structural size for transonic flight is excessively costly. The analysis of the governing physics is expensive, in particular for highly flexible aircraft, and the search for optima using a
Externí odkaz:
https://doaj.org/article/0d14e206f3294f47a72f6b5c288bc536
Publikováno v:
Shock and Vibration, Vol 9, Iss 3, Pp 105-121 (2002)
Proper orthogonal decomposition (POD) based reduced-order modelling is demonstrated to be a weighted residual technique similar to Galerkin's method. Estimates of weighted residuals of neglected modes are used to determine relative importance of negl
Externí odkaz:
https://doaj.org/article/512ed382aba448e0bc04d104b72be550
Publikováno v:
Theoretical and Applied Mechanics Letters, Vol 4, Iss 3 (2014)
In this paper, we investigate the role of morphing on flight dynamics of two birds by simulating the flow over rigid and morphing wings that have the characteristics of two different birds, namely the Giant Petrel and Dove Prion. The simulation of a
Externí odkaz:
https://doaj.org/article/195e11cfe36c429da3fdd55feddec3c2
Publikováno v:
International Journal of Computational Fluid Dynamics. 36:618-640
Autor:
Eliot S. Rudnick-Cohen, Joshua D. Hodson, Gregory W. Reich, Alexander M. Pankonien, Philip S. Beran
Publikováno v:
Journal of Aircraft. 59:861-874
Autor:
Markus P. Rumpfkeil, Philip S. Beran
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA Journal. 58:4764-4780
This work proposes a multifidelity modeling approach for predicting aeroelastic flutter of airfoils and wings. Using aerodynamic models based on the doublet-lattice method and time-accurate Euler e...
Autor:
David S. Makhija, Philip S. Beran
Publikováno v:
Structural and Multidisciplinary Optimization. 62:1275-1297
Autor:
Markus P. Rumpfkeil, Philip S. Beran
Publikováno v:
AIAA Journal. 58:1292-1303
Multifidelity sparse polynomial chaos expansion (MFSPCE) models of critical flutter dynamic pressures as a function of Mach number, angle of attack, and thickness-to-chord ratio are constructed in ...
Autor:
Markus P. Rumpfkeil, Philip S. Beran
Publikováno v:
AIAA SCITECH 2022 Forum.