| Nome |
# |
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An Airfoil Shape Optimization Technique coupling PARSEC Parameterization and Evolutionary Algorithm, file e268a72c-d745-4c8f-e053-1705fe0a812c
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3.323
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Design and integration sensitivity of a morphing trailing edge on a reference airfoil: The effect on high-altitude long-endurance aircraft performance, file e268a72f-1a15-4c8f-e053-1705fe0a812c
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335
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Design and aerodynamic analysis of a regional turboprop innovative configuration, file e268a72f-1ad9-4c8f-e053-1705fe0a812c
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300
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Noise, emissions and costs trade factors for regional jet platforms using a new software for aircraft preliminary design, file e268a731-e271-4c8f-e053-1705fe0a812c
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260
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AIRCRAFT DIRECTIONAL STABILITY AND CONTROL: NEW IMPROVED APPROACH IN TAIL DESIGN, file e268a72f-1c3a-4c8f-e053-1705fe0a812c
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183
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Advanced turboprop multidisciplinary design and optimization within agile project, file e268a730-0ac1-4c8f-e053-1705fe0a812c
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172
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null, file e268a730-0e16-4c8f-e053-1705fe0a812c
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150
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The Enabling Technologies for a Quasi-Zero Emissions Commuter Aircraft, file e268a733-8adc-4c8f-e053-1705fe0a812c
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138
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Retrofitting Cost Modeling in Aircraft Design, file 5b426d1f-0e93-471b-856a-28579373e2d0
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135
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Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project, file e268a730-07c1-4c8f-e053-1705fe0a812c
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130
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A Java toolchain of programs for aircraft design, file e268a72f-1583-4c8f-e053-1705fe0a812c
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112
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Innovative tools for aircraft preliminary design – development, applications and education, file e268a72f-1a91-4c8f-e053-1705fe0a812c
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87
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MDO applications to conventional and novel turboprop aircraft within agile European project, file e268a730-0e15-4c8f-e053-1705fe0a812c
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67
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Enhancing optimization capabilities using the AGILE collaborative MDO framework with application to wing and nacelle design, file e268a731-e639-4c8f-e053-1705fe0a812c
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65
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An improved method for transport aircraft for high lift aerodynamic prediction, file e268a72f-11ad-4c8f-e053-1705fe0a812c
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61
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Low Speed Take-Off Aerodynamic Analysis, file e268a72f-1adb-4c8f-e053-1705fe0a812c
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60
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Development of a Java-Based Framework for Aircraft Preliminary Design and Optimization, file e268a72e-048d-4c8f-e053-1705fe0a812c
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45
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Streamlining Cross-Organizational Aircraft Development: Results from the AGILE Project, file e268a730-b7b4-4c8f-e053-1705fe0a812c
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45
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Collaborative Design of a Business Jet Family Using the AGILE 4.0 MBSE Environment, file c9a15f16-edee-4b52-8299-5c2426fc4357
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36
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Effect of Progressive Integration of On-Board Systems Design Discipline in an MDA Framework for Aircraft Design with Different Level of Systems Electrification, file e268a733-9f4e-4c8f-e053-1705fe0a812c
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31
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Multidisciplinary Design and Optimization of Regional Jet Retrofitting Activity, file 1cc391d7-89e7-43b2-bd4e-71d5a7fb0e25
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22
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Multidisciplinary design of a more electric regional aircraft including certification constraints, file 5a3d3fe4-3c04-4de9-a487-d0fe9756909d
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20
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Numerical high lift prediction on the JAXA standard model, file e268a730-0e18-4c8f-e053-1705fe0a812c
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20
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Commuter aircraft aerodynamic design: wind-tunnel tests and CFD analysis, file e268a72c-d7cb-4c8f-e053-1705fe0a812c
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14
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Game theory and evolutionary algorithms applied to MDO in the AGILE European project, file e268a72e-c443-4c8f-e053-1705fe0a812c
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14
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A comprehensive review of vertical tail design, file e268a72e-4fce-4c8f-e053-1705fe0a812c
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13
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Flight Tests, Performances and Flight Certification of a Twin-Engine Light Aircraft, file e268a72c-cb24-4c8f-e053-1705fe0a812c
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11
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Design and aerodynamic analysis of a twin-engine commuter aircraft, file e268a72c-d42d-4c8f-e053-1705fe0a812c
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11
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Aircraft directional stability and vertical tail design: A review of semi-empirical methods, file e268a72f-1d00-4c8f-e053-1705fe0a812c
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10
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A Nash equilibrium-genetic algorithm optimization code for structural problems. test case: an aluminum plate subjected to low velocity impact events., file e268a72c-c6b7-4c8f-e053-1705fe0a812c
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9
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Flight tests, performances, and flight certification of a twin-engine light aircraft, file e268a72c-cd97-4c8f-e053-1705fe0a812c
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9
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Feasibility study of innovative regional turboprop: an overview of the European project IRON, file e268a731-6de8-4c8f-e053-1705fe0a812c
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9
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Design of hybrid-electric aircraft with fault-tolerance considerations, file e5781477-85dc-498e-b8b1-2d119063d062
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9
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Aero-Propulsive Interactions between UAV Wing and Distributed Propellers Due to Their Relative Position, file a4a9ecb1-7dca-408e-85b9-eefff398008f
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8
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Regional jet retrofitting design: from stakeholders’ needs and system’s requirements to MDAO workflow formulation, file cbc03ac3-ae4c-4ab5-927b-3d4d50050696
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8
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Stability, Flying Qualities and Parameter Estimation of a Twin-Engine CS23/FAR23 Certified Light Aircraft, file e268a72c-cb25-4c8f-e053-1705fe0a812c
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8
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Aerodynamic analysis and design of a twin engine commuter aircraft, file e268a72c-d1ee-4c8f-e053-1705fe0a812c
|
7
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A Java desktop application for Aircraft Preliminary Design, file e268a72e-6c82-4c8f-e053-1705fe0a812c
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7
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Development of new preliminary design methodologies for regional turboprop aircraft by CFD analyses, file e268a72c-d7ca-4c8f-e053-1705fe0a812c
|
6
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Aircraft Directional Stability Prediction method by CFD, file e268a72e-0915-4c8f-e053-1705fe0a812c
|
6
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A comprehensive review of vertical tail design, file e268a72e-d215-4c8f-e053-1705fe0a812c
|
6
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Aerodynamic analysis and optimization of a regional transport aircraft, file e268a72c-cc0d-4c8f-e053-1705fe0a812c
|
5
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CFD sensitivity analysis on bumped airfoil characteristics
for inflatable winglet, file e268a72c-d747-4c8f-e053-1705fe0a812c
|
5
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Numerical Aerodynamic Analysis of a New Twin Engine Commuter Aircraft, file e268a72e-685b-4c8f-e053-1705fe0a812c
|
5
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Methodological enhancements in MDO process investigated in the AGILE European project, file e268a72e-d21f-4c8f-e053-1705fe0a812c
|
5
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Powered wind tunnel tests setup of the IRON innovative turboprop aircraft, file e268a731-1a91-4c8f-e053-1705fe0a812c
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5
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A Nash equilibrium-genetic algorithm optimization code for structural problems. test case: an aluminum plate subjected to low velocity impact events., file e268a72c-c8a9-4c8f-e053-1705fe0a812c
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4
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Fuselage aerodynamic prediction methods, file e268a72e-0487-4c8f-e053-1705fe0a812c
|
4
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An Investigation on Vertical Tailplane Design, file e268a72c-d321-4c8f-e053-1705fe0a812c
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3
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Numerical aerodynamic analysis on a trapezoidal wing with high lift devices: a comparison with experimental data, file e268a72c-d746-4c8f-e053-1705fe0a812c
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3
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Aerodynamic interference issues in aircraft directional control, file e268a72e-0d83-4c8f-e053-1705fe0a812c
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3
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Wind tunnel testing of a generic regional turboprop aircraft modular model and development of improved design guidelines, file e268a730-0c9a-4c8f-e053-1705fe0a812c
|
3
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Design Guidelines for High Capacity Innovative Regional Turboprop Aircraft, file e268a730-0e1a-4c8f-e053-1705fe0a812c
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3
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Development of new preliminary design methodologies for regional turboprop aircraft by CFD analyses, file e268a731-b76f-4c8f-e053-1705fe0a812c
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3
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Hybridization and Mission Analysis of a regional turboprop, file e268a733-4686-4c8f-e053-1705fe0a812c
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3
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Aircraft conceptual design including powertrain system architecture and distributed propulsion, file 31c17638-c593-4ff0-b3bd-8143c64aa6db
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2
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Multi-Objective Bayesian Optimization With Mixed-Categorical Design Variables For Expensive-To-Evaluate Aeronautical Applications, file 33ddc8e7-ac5a-4ad5-a109-c4888125bee8
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2
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Diffuser shape optimization for GEM, a tethered system based on two horizontal axis hydro turbines, file e268a72e-0bc8-4c8f-e053-1705fe0a812c
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2
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Aerodynamic design and analysis of an innovative regional turboprop configuration, file e268a730-0a88-4c8f-e053-1705fe0a812c
|
2
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|
An improved high‑lift aerodynamic prediction method for transport aircraft, file e268a730-0abf-4c8f-e053-1705fe0a812c
|
2
|
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Application of game theory and evolutionary algorithm to the regional turboprop aircraft wing optimization, file e268a730-0ad3-4c8f-e053-1705fe0a812c
|
2
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High performance computing (HPC) and aerospace research activities at the University of Naples Federico II, file e268a730-f461-4c8f-e053-1705fe0a812c
|
2
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Automatic modeling of aircraft external geometries for preliminary design workflows, file e268a731-d487-4c8f-e053-1705fe0a812c
|
2
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Aircraft conceptual design including powertrain system architecture and distributed propulsion, file 1e25f72d-d7d5-4f27-8af2-cef4febd2375
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1
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WORKSHOP Internazionale COMMUTER AND REGIONAL HYBRID-ELECTRIC
AIRCRAFT DESIGN 6-7 October 2022 Location : Via Partenope,36 University Congress Centre, NAPLES.
https://www.smartup-engineering.com/workshop/, file 21c8b996-08d7-4830-ab15-d34d85d8c598
|
1
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An investigation on vertical tailplane contribution to aircraft sideforce, file 4978c3fd-c67b-46bc-9752-c2365d453f69
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1
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Aerodynamic interference issues in aircraft directional control, file e268a72c-d74a-4c8f-e053-1705fe0a812c
|
1
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A New Vertical Tail Design Procedure for General Aviation and Turboprop Aircraft, file e268a72c-d820-4c8f-e053-1705fe0a812c
|
1
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Commuter aircraft aerodynamic characteristics through wind tunnel tests, file e268a72e-0482-4c8f-e053-1705fe0a812c
|
1
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Aerodynamic guidelines in the design and optimization of new regional turboprop aircraft, file e268a72e-0eae-4c8f-e053-1705fe0a812c
|
1
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Innovative turbopROp configuration (IRON), file e268a72e-1ec7-4c8f-e053-1705fe0a812c
|
1
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Roll performance assessment of a light aircraft: Flight simulations and flight tests, file e268a730-036b-4c8f-e053-1705fe0a812c
|
1
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Performance evaluation and DOC estimation of an innovative turboprop configuration, file e268a730-0c9d-4c8f-e053-1705fe0a812c
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1
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Numerical analysis of propeller effects on wing aerodynamic: Tip mounted and distributed propulsion, file e268a730-2547-4c8f-e053-1705fe0a812c
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1
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High lift aerodynamic characteristics of a three lifting surfaces turboprop aircraft, file e268a730-a44a-4c8f-e053-1705fe0a812c
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1
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Longitudinal stability issues including propulsive effects on an innovative commercial propeller-driven aircraft, file e268a730-e20e-4c8f-e053-1705fe0a812c
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1
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Aerodynamic Design Guidelines of Aircraft Dorsal Fin, file e268a731-9cef-4c8f-e053-1705fe0a812c
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1
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Aeroelastic wind tunnel tests of the RIBES wing model, file e268a731-b75c-4c8f-e053-1705fe0a812c
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1
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| Totale |
6.047 |