Items where Author is "Akbar, Mahesa"

[Atom feed] Atom [RSS2 feed] RSS
Group by: Item Type | Full Text | No Grouping
Jump to: Public | None
Number of items: 13.

Public

file
JUSUF, Annisa, JARWADI, Maulana Hayu, HASTUNGKOROJATI, Dhimaz Galang, GUNAWAN, Leonardo, AKBAR, Mahesa, ZAKARIA, Kemas, IZZATURRAHMAN, Muhammad Faiz and PALAR, Pramudita Satria (2024). Design Exploration and Optimization of a Multi-Corner Crash Box under Axial Loading via Gaussian Process Regression. International Journal of Technology, 15 (6), 1749-1770. [Article]

file
RAMADHAN, Faisal, SASONGKO, Rianto Adhy, GUNAWAN, Leonardo, AKBAR, Mahesa and WIDAGDO, Djarot (2024). The Effect of Fiber Orientation and Crack on Dynamic Characteristics of a Unidirectional Composite Cantilevered Wing Plate. International Journal of Technology, 15 (6), 1663-1667. [Article]

file
WIRAWAN, Nanda, ABUZAYED, Ibrahim H., AKBAR, Mahesa and CURIEL-SOSA, Jose L. (2024). Robust Fast Fracture Plane Orientation Angle Search Algorithm for Puck 3D Inter-Fibre Failure Criterion. European Journal of Computational Mechanics, 227-254. [Article]

file
KEVIN, Alexander, AKBAR, Mahesa, GUNAWAN, Leonardo, AULIA, Darryl Khalid, AGUNG, Rizqy, RAWIKARA, Seno Sahisnu, SASONGKO, Rianto Adhy and WIDAGDO, Djarot (2023). Evaluation of Piezoelectric-based Composite for Actuator Application via FEM with Thermal Analogy. European Journal of Computational Mechanics. [Article]

file
AKBAR, Mahesa, RAMADHANI, Mileniawan Januar, IZZUDDIN, Mohammad Arif, GUNAWAN, Leonardo, SASONGKO, Rianto Adhy, KUSNI, Muhammad and CURIEL-SOSA, Jose Luis (2022). Evaluation on Piezoaeroelastic Energy Harvesting Potential of A Jet Transport Aircraft Wing with Multiphase Composite by means of Iterative Finite Element Method. International Journal of Technology, 13 (4), 803-815. [Article]

file
DEASTRA, Predaricka, WAGG, David, SIMS, Neil and AKBAR, Mahesa (2020). Tuned inerter dampers with linear hysteretic damping. Earthquake Engineering & Structural Dynamics, 49 (12), 1216-1235. [Article]

file
AKBAR, Mahesa and CURIEL-SOSA, Jose Luis (2018). Evaluation of piezoelectric energy harvester under dynamic bending by means of hybrid mathematical/isogeometric analysis. International Journal of Mechanics and Materials in Design, 14 (4), 647-667. [Article]

file
AHMAD, MIM, CURIEL-SOSA, JL, AKBAR, Mahesa and ABDULLAH, NA (2018). Numerical Inspection based on Quasi-Static Analysis using Rousselier Damage Model for Aluminium Wingbox Aircraft Structure. Journal of Physics: Conference Series, 1106: 012013. [Article]

file
ABDULLAH, Nur Azam, CURIEL-SOSA, Jose Luis and AKBAR, Mahesa (2018). Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method. Composite Structures, 202, 151-161. [Article]

file
WIRAWAN, N, ABDULLAH, NA, AKBAR, Mahesa and CURIEL-SOSA, JL (2018). Analysis on Cracked Commuter Aircraft Wing Under Dynamic Cruise Load By Means of XFEM. Journal of Physics: Conference Series, 1106: 012014. [Article]

file
AKBAR, Mahesa and CURIEL-SOSA, JL (2016). Piezoelectric energy harvester composite under dynamic bending with implementation to aircraft wingbox structure. Composite Structures, 153, 193-203. [Article]

None

AHMAD, M.I.M., AKBAR, Mahesa and ABDULLAH, N.A. (2023). Development of constitutive creep damage-based modified Robinson–Rousselier (MRR) model with XFEM for void-crack relation in ductile materials. Mechanics of Time-Dependent Materials, 27 (4), 1069-1095. [Article]

ABDULLAH, Nur Azam, AKBAR, Mahesa, WIRAWAN, Nanda and CURIEL-SOSA, Jose Luis (2019). Structural integrity assessment on cracked composites interaction with aeroelastic constraint by means of XFEM. Composite Structures, 229: 111414. [Article]

This list was generated on Wed Mar 12 23:56:57 2025 UTC.