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.
- Unstructured Shock-Fitting Calculations of the Transonic Flow in a Gas Turbine Cascade
- Finite elements with node dependent kinematics and scalable accuracy for the analysis...
- On-Board Telemetry Monitoring via Support Vector Machine with Application to Philae...
- Design, Optimization and Manufacturing of Metallic Wings of Light Aircraft
- CFD Rebuilding of Cold Hypersonic Flow in GHIBLI facility
- Preliminary design of a Tiltwing UAV with a box wing configuration
- Preliminary analysis of the HEXAFLY-International Vehicle
- Optimization of low-thrust trajectory for a mission to the asteroid 433 Eros with Earth...
- Occupants’ Injury during a Drop Test of an Advanced Composite Fuselage Section
- The LARES 2 satellite: new challenges for design and ground test
- The use of RANS approach for predicting transition
- Frozen Sonic Flow Method Applied to Arc-Heated Facilities for Planetary Re-Entry...
- Development and Validation of Simplied 1D Models for Hollow Cathode Analysis and Design
- Selecting Optimal Inspection Trajectories For Target Observation
- Elastoplastic and progressive failure analysis of fiber-reinforced composites via an...
- Multi-objective Optimization for the Design of an Unconventional Sun-Powered...
- Numerical study of 3D gaseous detonations in a square channel
- Design of a Fuselage-Mounted Main Landing Gear of a Medium-Size Civil Transport Aircraft
- A Pilot mental workload case study in a Full Flight Simulator
- First Steps Towards a Digital Plane Wave Superposition Method for Vibroacoustic Problems
- PERFORMANCE ANALYSIS AND GAINS TUNING PROCEDURE FOR A CONTROLLED SPACE MANIPULATOR USED...
- Unsteady 1-D Thrust Modeling with EOS Effects for Ram Accelerator Experiments at...
- PARSIFAL Project: a breakthrough innovation in air transport
- NUMERICAL INVESTIGATION ON DELAMINATION GROWTH IN COMPOSITE PANELS INCLUDING...
- Mathematics of attitude-constrained optimal low-thrust orbit transfer