Aerotecnica Missili & Spazio

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AIDAA News #15
Aerotecnica Missili & Spazio - Tập 101 - Trang 305-306 - 2022
Marco Petrolo
Evaluation of the Biomechanical Responses During an Aircraft Emergency Landing
Aerotecnica Missili & Spazio - Tập 101 - Trang 121-133 - 2022
Giovanna Fusco
Passengers’ safety in unconventional situations, such as those of an emergency landing, has become more and more important due to the increase of air traffic. To improve passengers’ safety, certification authorities have imposed specific crashworthiness requirements in airworthiness regulations as defined in Title 14 of Federal Regulations Code—Part 25 for transport aircraft. Over the years, a ser...... hiện toàn bộ
Non-linear modelling for Multi-Disciplinary and Multi-Objective Optimization of a complete aircraft
Aerotecnica Missili & Spazio - Tập 92 Số 1-2 - Trang 61-68 - 2013
Stefania Gemma, Franco Mastroddi
Reliability Centered Maintenance Analysis Using Analytic Hierarchy Process for Electro-mechanical Actuators
Aerotecnica Missili & Spazio - Tập 100 - Trang 321-335 - 2021
Deniz Can Doğan, Yusuf Tansel İç
There is an increasing trend for the usage of electrically powered equipment in the aviation industry. In this paper, a Reliability Centered Maintenance (RCM) analysis application is performed for Electro-Mechanical Actuators (EMA). We consider a new model for criticality classification for individual failure modes for the Reliability Centered Maintenance analysis stages using the Analytic Hierarc...... hiện toàn bộ
AIDAA News #11
Aerotecnica Missili & Spazio - Tập 100 - Trang 289-290 - 2021
Sergio De Rosa
Evaluation of Regression Rate Enhancing Concepts and Techniques for Hybrid Rocket Engines
Aerotecnica Missili & Spazio - - 2022
Christopher Glaser, Jouke Hijlkema, J. Anthoine
AbstractThe low regression rate of Hybrid Rocket Engines (HREs) is one prominent characteristic that is addressed in most abstracts concerning hybrid propulsion. Over the years, researchers developed and investigated numerous ways to tackle the low regression rate problem of HREs. This article is a collection and assessment of these diverse methods and designs. It ...... hiện toàn bộ
A global exploration method to identify families of cycling Earth–Mars trajectories
Aerotecnica Missili & Spazio - Tập 99 Số 3 - Trang 187-194 - 2020
E. Fornari, Mauro Pontani
Determining Dynamic Stability of a Re-entry Capsule at Free Fall
Aerotecnica Missili & Spazio - - Trang 1-16 - 2023
C. Priyant Mark, Winston Netto
Re-entry capsules, designed with blunt-body shapes to endure hypersonic air velocities and heat, encounter instability in the low subsonic regime during the final descent phase. Ensuring a controlled descent with the appropriate attitude for deploying deceleration systems becomes paramount. To address this challenge, we employ a cost-effective approach to investigate the dynamic stability of a typ...... hiện toàn bộ
Preface
Aerotecnica Missili & Spazio - Tập 98 - Trang 173-173 - 2019
Marco Vezza
Ultralight amphibious PrandtlPlane: the final design
Aerotecnica Missili & Spazio - Tập 95 - Trang 125-135 - 2016
V. Cipolla, A. Frediani, F. Oliviero, R. Rossi, E. Rizzo, M. Pinucci
The IDINTOS project, co-founded by the Regional Government of Tuscany (Italy), concerns the design of a ultralight amphibious PrandtlPlane and the manufacturing of a flying prototype. A consortium of universities and private companies participated to the project, coordinated by University of Pisa. The paper describes the general design of the aircraft, including aerodynamics, hydrodynamics, struct...... hiện toàn bộ
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