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Tarik H. Orra
Tarik H. Orra
ADASI
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SUAVE: an open-source environment for multi-fidelity conceptual vehicle design
TW Lukaczyk, AD Wendorff, M Colonno, TD Economon, JJ Alonso, ...
16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 3087, 2015
1492015
Suave: An open-source environment for conceptual vehicle design and optimization
EM Botero, A Wendorff, T MacDonald, A Variyar, JM Vegh, TW Lukaczyk, ...
54th AIAA Aerospace Sciences Meeting, 1275, 2016
552016
SUAVE: An open-source Environment enabling unconventional vehicle designs through higher fidelity
T MacDonald, E Botero, JM Vegh, A Variyar, JJ Alonso, TH Orra, ...
55th AIAA Aerospace sciences meeting, 0234, 2017
242017
Multi-objective aircraft design optimization for low external noise and fuel burn
CR Ilario da Silva, TH Orra, JJ Alonso
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017
122017
Flight Path and Wing Optimization of Lithium-Air Battery Powered Passenger Aircraft
JM Vegh, JJ Alonso, TH Orra, C Ilario da Silva
53rd AIAA Aerospace Sciences Meeting, 1674, 2015
122015
SUAVE: An Aerospace Vehicle Environment for Designing Future Aircraft
A Wendorff, A Variyar, C Ilario, E Botero, F Capristan, J Smart, J Alonso, ...
Stanford University Aerospace Design Lab, 2020
82020
The impact on production and costs after the acquisition of an airline by a competitor in Brazil: a Cobb-Douglas function application
JATG Fregnani, TH Orra, RAG Eller, BS de Mattos
TRANSPORTES 27 (1), 172-183, 2019
62019
Evaluation of the Impacts of Objective Function Definition in Aircraft Conceptual Design
DHB Di Bianchi, TH Orra, FJ Silvestre
Journal of Aircraft 55 (3), 1231-1243, 2018
52018
Optimization Under Uncertainty: Rethinking Margins at the Conceptual Design
D Bianchi, TH Orra, C Silva, FJ Silvestre
2018 Multidisciplinary Analysis and Optimization Conference, 3104, 2018
32018
Monte Carlo based Robust MDO applied to Aircraft Conceptual Design: a technical-financial coupling optimization strategy
D Bianchi, TH Orra, P Paglione
15th AIAA Aviation Technology, Integration, and Operations Conference, 2737, 2015
32015
Unmanned aircraft having reduced acoustic signatures
RFG Ribeiro, TH Orra
US Patent 11,597,514, 2023
22023
A Semi-Empirical Methodology for Balanced Field Length Estimation of Jet-Engined Aircraft in Early Design Phases
T Angeiras
5th CEAS Air and Space Conference: Challenges in European Aerospace, 2015
22015
Surrogate Modeling to Enable Higher Fidelity Optimization
JM Vegh, JJ Alonso, CR Ilario da Silva, TH Orra
18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 3661, 2017
12017
Unmanned aircraft
RFG Ribeiro, TH Orra
US Patent App. 29/702,045, 2024
2024
Wing airfoil geometric parametrization method for efficient aerodynamic design optimization
RF de Souza, APC Cuco, TH Orra
17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 3670, 2016
2016
Handling qualities evaluation of a VMCG reduction functionality
TH Orra, LR Cruz, MF Oliveira
AIAA Atmospheric Flight Mechanics (AFM) Conference, 4504, 2013
2013
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Artiklar 1–16