Aerotecnica Missili & Spazio
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Aerotecnica Missili e Spazio is the journal of the Italian Association of Aeronautics and Astronautics, AIDAA,founded in 1920. The journal aims at publishing contributions in the field of aerospace sciences, technologies and systems. This includes disciplines in the area of mechanical sciences like flight mechanics, aerodynamics, propulsion, aerothermochemistry, structures and materials, astrodynamics as well as other disciplines such as telecommunication, navigation, control, electronics, informatics and all aspects related to ground testing and operations when applied to the aerospace field. Contributions regarding the aeronautical or space vehicle as an engineering system are particularly welcome. Also in covering the basic disciplines here above recalled, submitted manuscripts should always address the aerospace missions and systems rather than strictly specialized topics more appropriate to a discipline oriented journal. Paper dealing with overall exploitation and management of aerospace systems and on the impact of scientific applications on system design and operation, as an example in the fields of remote sensing, microgravity, geodesy, exploration and astrophysics, are encouraged too. Aerotecnica Missili e Spazio welcomes scientific contributions that provide a clear novelty in their field and assesses the quality of the papers by a strict peer review process under the supervision of the editor supported by an international editorial board of experts.
- Aerodynamic optimization of a large PrandtlPlane configuration
- Optimal and robust design of a control surface actuation system within the GLAMOUR project
- Tests of Sapphire Optical Fiber Sensors for Strain Monitoring in High Temperature...
- Aeroelastic Rotorcraft-Pilot Couplings: Problems and Methods
- Flight dynamics model for preliminary design of PrandtlPlane wing configuration with...
- Artificial Equilibrium Orbital Configurations by Means of Continuous Thrust
- Analyses of non local effects of riblets
- Analysis of non-classical aileron buzz
- Analysis on aerodynamic characteristics of a paraglider airfoil
- Numerical Simulation of Fluidic Thrust-Vectoring
- Stability analysis of three-dimensional laminar compressible boundary layers based in...
- Ultralight amphibious PrandtlPlane: the final design
- Aerodynamic Boundary Element Method for Bluff Bodies with Wind Tunnel Data Correlation
- Magnetic Spacecraft Control via Output Feedback with Separation between Measurement and...
- Effect of gas-phase carbon depletion by sooting on the structure of methane/air flamelets
- Space Carbon-Carbon Thermal Protection System Electromagnetic Characterization in...
- Framework of Conceptual Design Methodology for Hybrid Buoyant Aircraft
- A New, General Perturbative Guidance for Space Vehicles
- Semi-Analytical Orbital Parameters Description for Thermal Fatigue Analysis
- Evaluation of Main Parameters in Re-Entry Trajectories
- Analysis of distorted similitudes for the frequency response of composite plates
- Exact Solutions for Dynamic and Quasi-Static Thermoelasticity Problems in Rotating Disks
- High Thickness Kevlar/Carbon Nanostructured Composite for Impact Protection
- Variational Approach to the Problem of the Optimal Propeller Design
- Il 44esimo Salone Internazionale dell’Aeronautica e dello Spazio di Le Bourget