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  Subjects -> AERONAUTICS AND SPACE FLIGHT (Total: 123 journals)
Showing 1 - 30 of 30 Journals sorted alphabetically
Acta Astronautica     Hybrid Journal   (Followers: 496)
Advances in Aerospace Engineering     Open Access   (Followers: 70)
Advances in Aerospace Science and Technology     Open Access   (Followers: 8)
Advances in Astronautics Science and Technology     Hybrid Journal   (Followers: 1)
Advances in Space Research     Full-text available via subscription   (Followers: 458)
Aeronautical Journal, The     Hybrid Journal   (Followers: 13)
Aerospace     Open Access   (Followers: 60)
Aerospace Medicine and Human Performance     Full-text available via subscription   (Followers: 19)
Aerospace Science and Technology     Hybrid Journal   (Followers: 430)
Aerospace Scientific Journal     Open Access   (Followers: 18)
Aerospace Systems     Hybrid Journal   (Followers: 6)
Aerospace technic and technology     Open Access   (Followers: 3)
Aerotecnica Missili & Spazio : Journal of Aerospace Science, Technologies & Systems     Hybrid Journal   (Followers: 4)
AIAA Journal     Hybrid Journal   (Followers: 1196)
Air Force Magazine     Full-text available via subscription   (Followers: 10)
Air Medical Journal     Hybrid Journal   (Followers: 8)
Aircraft Engineering and Aerospace Technology     Hybrid Journal   (Followers: 264)
Annual of Navigation     Open Access   (Followers: 22)
Artificial Satellites     Open Access   (Followers: 23)
ASTRA Proceedings     Open Access   (Followers: 3)
Astrodynamics     Hybrid Journal   (Followers: 4)
Aviation     Open Access   (Followers: 17)
Aviation Advances & Maintenance     Open Access   (Followers: 5)
Aviation in Focus - Journal of Aeronautical Sciences     Open Access   (Followers: 10)
Aviation Psychology and Applied Human Factors     Hybrid Journal   (Followers: 27)
Aviation Week     Full-text available via subscription   (Followers: 438)
Canadian Aeronautics and Space Journal     Full-text available via subscription   (Followers: 34)
CEAS Aeronautical Journal     Hybrid Journal   (Followers: 30)
Chinese Journal of Aeronautics     Open Access   (Followers: 21)
Ciencia y Poder Aéreo     Open Access   (Followers: 2)
Civil Aviation High Technologies     Open Access   (Followers: 5)
Control Systems     Hybrid Journal   (Followers: 315)
Cosmic Research     Hybrid Journal   (Followers: 5)
COSPAR Colloquia Series     Full-text available via subscription   (Followers: 11)
Egyptian Journal of Remote Sensing and Space Science     Open Access   (Followers: 24)
Elsevier Astrodynamics Series     Full-text available via subscription   (Followers: 12)
Fatigue of Aircraft Structures     Open Access   (Followers: 15)
Frontiers in Astronomy and Space Sciences     Open Access   (Followers: 12)
Gravitational and Space Research     Open Access  
Gyroscopy and Navigation     Hybrid Journal   (Followers: 260)
IEEE Aerospace and Electronic Systems Magazine     Full-text available via subscription   (Followers: 279)
IEEE Journal on Miniaturization for Air and Space Systems     Hybrid Journal   (Followers: 2)
IEEE Transactions on Aerospace and Electronic Systems     Hybrid Journal   (Followers: 385)
IEEE Transactions on Circuits and Systems I: Regular Papers     Hybrid Journal   (Followers: 39)
International Journal of Aeroacoustics     Hybrid Journal   (Followers: 41)
International Journal of Aerodynamics     Hybrid Journal   (Followers: 37)
International Journal of Aeronautical and Space Sciences     Hybrid Journal   (Followers: 2)
International Journal of Aerospace Engineering     Open Access   (Followers: 82)
International Journal of Aerospace Psychology     Hybrid Journal   (Followers: 23)
International Journal of Aerospace Sciences     Open Access   (Followers: 32)
International Journal of Applied Geospatial Research     Hybrid Journal   (Followers: 7)
International Journal of Aviation Management     Hybrid Journal   (Followers: 9)
International Journal of Aviation Technology, Engineering and Management     Full-text available via subscription   (Followers: 7)
International Journal of Aviation, Aeronautics, and Aerospace     Open Access   (Followers: 5)
International Journal of Crashworthiness     Hybrid Journal   (Followers: 12)
International Journal of Micro Air Vehicles     Full-text available via subscription   (Followers: 11)
International Journal of Satellite Communications Policy and Management     Hybrid Journal   (Followers: 13)
International Journal of Space Science and Engineering     Hybrid Journal   (Followers: 11)
International Journal of Space Structures     Full-text available via subscription   (Followers: 17)
International Journal of Space Technology Management and Innovation     Full-text available via subscription   (Followers: 10)
International Journal of Sustainable Aviation     Hybrid Journal   (Followers: 5)
International Journal of Turbo and Jet-Engines     Hybrid Journal   (Followers: 6)
Investigación Pecuaria     Open Access   (Followers: 3)
Journal of Aerodynamics     Open Access   (Followers: 18)
Journal of Aeronautical Materials     Open Access   (Followers: 9)
Journal of Aeronautics & Aerospace Engineering     Open Access   (Followers: 31)
Journal of Aerospace Engineering     Full-text available via subscription   (Followers: 69)
Journal of Aerospace Engineering & Technology     Full-text available via subscription   (Followers: 18)
Journal of Aerospace Information Systems     Hybrid Journal   (Followers: 22)
Journal of Aerospace Information Systems     Hybrid Journal   (Followers: 34)
Journal of Aerospace Technology and Management     Open Access   (Followers: 7)
Journal of Aircraft     Hybrid Journal   (Followers: 337)
Journal of Aircraft and Spacecraft Technology     Open Access   (Followers: 9)
Journal of Airline and Airport Management     Open Access   (Followers: 12)
Journal of Astrobiology & Outreach     Open Access   (Followers: 3)
Journal of Aviation Technology and Engineering     Open Access   (Followers: 11)
Journal of Aviation/Aerospace Education & Research     Open Access   (Followers: 2)
Journal of Engineering and Technological Sciences     Open Access   (Followers: 1)
Journal of Guidance, Control, and Dynamics     Hybrid Journal   (Followers: 205)
Journal of KONBiN     Open Access   (Followers: 3)
Journal of Navigation     Hybrid Journal   (Followers: 280)
Journal of Propulsion and Power     Hybrid Journal   (Followers: 615)
Journal of Space Safety Engineering     Hybrid Journal   (Followers: 8)
Journal of Space Weather and Space Climate     Open Access   (Followers: 27)
Journal of Spacecraft and Rockets     Hybrid Journal   (Followers: 773)
Journal of Spatial Science     Hybrid Journal   (Followers: 3)
Journal of the American Helicopter Society     Full-text available via subscription   (Followers: 8)
Journal of the Astronautical Sciences     Hybrid Journal   (Followers: 9)
Journal of the Australasian Society of Aerospace Medicine     Open Access   (Followers: 1)
Journal of Wind Engineering and Industrial Aerodynamics     Hybrid Journal   (Followers: 17)
Life Sciences in Space Research     Hybrid Journal   (Followers: 4)
MAD - Magazine of Aviation Development     Open Access   (Followers: 2)
Mekanika : Jurnal Teknik Mesin i     Open Access   (Followers: 1)
Microgravity Science and Technology     Hybrid Journal   (Followers: 2)
New Space     Hybrid Journal   (Followers: 6)
Nonlinear Dynamics     Hybrid Journal   (Followers: 20)
npj Microgravity     Open Access   (Followers: 3)
Open Aerospace Engineering Journal     Open Access   (Followers: 1)
Perspectives of Earth and Space Scientists i     Open Access  
Population Space and Place     Hybrid Journal   (Followers: 9)
Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa / Problems of Mechatronics. Armament, Aviation, Safety Engineering     Open Access   (Followers: 3)
Proceedings of the Human Factors and Ergonomics Society Annual Meeting     Hybrid Journal   (Followers: 16)
Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering     Hybrid Journal   (Followers: 46)
Progress in Aerospace Sciences     Full-text available via subscription   (Followers: 81)
Propulsion and Power Research     Open Access   (Followers: 68)
REACH - Reviews in Human Space Exploration     Full-text available via subscription   (Followers: 5)
Research & Reviews : Journal of Space Science & Technology     Full-text available via subscription   (Followers: 17)
RocketSTEM     Free   (Followers: 6)
Russian Aeronautics (Iz VUZ)     Hybrid Journal   (Followers: 24)
Science and Education : Scientific Publication of BMSTU     Open Access   (Followers: 1)
Space and Polity     Hybrid Journal   (Followers: 4)
Space Policy     Hybrid Journal   (Followers: 29)
Space Research Today     Full-text available via subscription   (Followers: 48)
Space Safety Magazine     Free   (Followers: 51)
Space Science International     Open Access   (Followers: 202)
Space Science Reviews     Hybrid Journal   (Followers: 97)
SpaceNews     Free   (Followers: 825)
Spatial Information Research     Hybrid Journal   (Followers: 1)
Technical Soaring     Full-text available via subscription   (Followers: 1)
Transport and Aerospace Engineering     Open Access   (Followers: 1)
Transportmetrica A : Transport Science     Hybrid Journal   (Followers: 9)
Unmanned Systems     Hybrid Journal   (Followers: 5)
Вісник Національного Авіаційного Університету     Open Access   (Followers: 2)

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Journal Cover
International Journal of Aerospace Sciences
Number of Followers: 32  

  This is an Open Access Journal Open Access journal
ISSN (Print) 2169-8872 - ISSN (Online) 2169-8899
Published by SAP Homepage  [105 journals]
  • 1U CubeSat Platform Design

    • Abstract: Publication year: 2020Source: International Journal of Aerospace Sciences, Volume 8, Number 1Nickolay ZosimovychThis paper surveys and estimates the potential of one-unit CubeSat platform and reflects about design a more suitable platform for future CubeSats. During CubeSat platform development, the concept of the design process is formulated and standard physical relationships are proposed to find number of optimal design solution in terms of basic limitations and features compatibility. Specifically, new modular structure is proposed in order to allows flexible subsystems settlement. A design analysis is also presented concerning the CubeSat platform manufacturing technique. A CubeSat structure has been realized by using a rapid prototyping technique. Such choice allows to optimize a CubeSat design, manufacture, and - assembly.
       
  • Partially Invariant System for Spacecraft Center of Mass Motion
           Stabilization

    • Abstract: Publication year: 2019Source: International Journal of Aerospace Sciences, Volume 7, Number 1Nickolay ZosimovychThis publication suggests how we can improve the spacecraft centre of mass movement stabilization accuracy in the active phases of trajectory correction. It will be during interplanetary and transfer flights, which in some cases provides for high navigation accuracy, when rigid trajectory control method is used. The required stability conditions obtained are consistent with the known criteria in the invariant theory. Computer modelling shows that in a partially invariant stabilization system reveals the significant advantages of such a system in terms of greater accuracy when compared to known stabilization systems.
       
  • Automated Preliminary Thermal and Stress Analyses Applied to a Turbine
           Housing Assembly

    • Abstract: Publication year: 2019Source: International Journal of Aerospace Sciences, Volume 7, Number 1M. Moret, H. Moustapha, Patricia Phutthavong, F. GarnierThe use of Multidisciplinary Design Optimization (MDO) techniques at the preliminary design phase (PMDO) of a gas turbine engine allows investing more effort at the pre-detailed phase in order to prevent the selection of an unsatisfactory concept early in the design process. Considering the impact of the turbine tip clearance on an engine’s efficiency, an accurate tool to predict the tip gap is a mandatory step towards the implementation of a full PMDO system for the turbine design. Tip clearance calculation is a good candidate for PMDO technique implementation considering that it implies various analyses conducted on both the rotor and stator. As a second step to the development of such tip clearance calculator satisfying PMDO principles, the present work explores the automation feasibility of the whole analysis phase of a turbine shroud segment and housing assembly preliminary design process, and the potential increase in the accuracy of results and time savings. The proposed conceptual system integrates a thermal boundary condition automated calculator and interacts with a simplified air system generator and with several design tools based on parameterized CAD models. Great improvements were found when comparing this analysis method results with regular pre-detailed level tools, as they revealed to be closer to the one generated by the detailed design tools used as target. Moreover, this design process revealed to be faster than a common preliminary design phase while leading to a reduction of time spent at the detailed design phase. By requiring fewer user inputs, this system decreases the risk of human error while entirely leaving the important decisions to the designer.
       
  • Developments in Angular Momentum Exchange

    • Abstract: Publication year: 2018Source: International Journal of Aerospace Sciences, Volume 6, Number 1Timothy Sands, Danni Lu, Janhwa Chu, Baolin ChengUnder the assumption of indifferently statics stability attitude controller is designed for the warhead based on Lyapunov theory. And also, a pseudo-inverse steering law with null motions is used to generate the gimbal velocity commands for SGCMGs, according to the desired torque from the attitude controller. Comparing with the strategies with fins or thrusters, the ablation of the actuators can be prevented and the aerodynamic shape can be preserved in this one since SGCMGs are mounted inside the warhead directly. Comparing with the moving mass or flywheels, SGCMGs can output torque large enough to meet the need of large-scope attitude reorientation and stabilization for the warhead. Simulation results using a Pershing II ballistic missile with a certain warhead indicate that the control strategy with SGCMGs is feasible. This document provides a technical translation from Chinese to English of recent developments to improve the ability of the mobile penetration, Single Gimbal Control Moment Gyroscopes (SGCMG) are adopted instead of the control fins and vector thrusters to produce the torque for the attitude control of the re-entry warhead. In addition to the technical translation, the manuscript is set in the broader context of the literature.
       
  • Modeling of Transition Processes in a Partially Invariant Center of Mass
           Motion Stabilization System

    • Abstract: Publication year: 2017Source: International Journal of Aerospace Sciences, Volume 5, Number 1Nickolay ZosimovychThe publication suggests how to significantly improve the spacecraft centre of mass movement stabilization accuracy in the active phases of trajectory correction during interplanetary and transfer flights, which in some cases provides for high navigation accuracy, when rigid trajectory control method is used. The required stability conditions obtained are consistent with the known criteria in the invariant theory. Computer modelling shows that in a partially invariant stabilization system reveals the significant advantages of such a system in terms of greater accuracy when compared to known stabilization systems.
       
  • Performance of GOE-387 Airfoil Using CFD

    • Abstract: Publication year: 2017Source: International Journal of Aerospace Sciences, Volume 5, Number 1Mohamed A. Fouad Kandil, Abdelrady Okasha ElnadyIn this research, CFD analysis of the two-dimensional subsonic flow over a GOE 387 airfoil at various angles of attack and operating at a Reynolds number of 3 x105 is presented. Pressure distribution, Pressure Coefficient (Cp), Moment Coefficient (Cm) Lift Coefficient (Cl), and Drag Coefficient (Cd) are determined. The geometry of the airfoil is created using ANSYS Design Modeler. CFD analysis is carried out using FLUENT 17.2 at various angles of attack from -5° to 20°. Pressure distributions over GOE-387 airfoil for different angles of attack are presented. Moment coefficients and pressure coefficients are plotted against the angle of attack. Cl-Cd graph is plotted.
       
  • Design and CFD Analysis of Airborne Wind Turbine for Boats and Ships

    • Abstract: Publication year: 2016Source: International Journal of Aerospace Sciences, Volume 4, Number 1Masoud Arabbeiki ZefrehWind energy is a promising alternative to the depleting non-renewable sources. Airborne wind turbine can reach much higher altitudes and produce higher power due to high wind velocity and energy density than the conventional wind turbines. The focus of this paper is to design a shrouded airborne wind turbine, capable of generating 70 kW to propel a leisure boat with a capacity of 8-10 passengers. The Solidworks model has been analyzed numerically CFD, by StarCCM+ software. At this moment, The Unsteady Reynolds Averaged Navier Stokes Simulation (URANS) has been analyzed. Turbulence model has been selected, to study the physical properties of the flow, with emphasis on the performance of the turbine and the increase in air velocity at the throat. The analysis has been done using two ambient velocities. For the first time, at inlet velocity of 12 m/s, the velocity of air at the turbine has been recorded as 16 m/s. The power generated by the turbine is 61 kW. For the second time, at inlet velocity of 6m/s, the velocity of air at turbine increased to 10 m/s. The power generated by turbine is 25 kW.
       
  • Performance of Epoxy and Nanodiamond Exfoliated Montmorillonite
           Nanocomposite

    • Abstract: Publication year: 2016Source: International Journal of Aerospace Sciences, Volume 4, Number 1Ayesha KausarThis report investigates the possibility of improving the mechanical properties of triglycidyl para-amino phenol (TGAP) epoxy through dispersion of nanodiamond (ND) and montmorillonite-nanodiamond (MMT-ND) filler. The montmorillonite was first intercalated with octadecylamine followed by nanodiamond intercalation to form MMT-ND. Both the pristine nanodiamond as well as MMT-ND was employed as filler to form nanocomposite with triglycidyl para-amino phenol. In this case, diethyltoluene diamine was used as hardener. It was found that the presence of nanofiller steadily decreased the β-transition temperature of TGAP/ND and TGAP/MMT-ND systems. Atomic force micrographs have shown fine particle dispersion in nanocomposite. The effect of filler concentration on mechanical properties of epoxy resins was also analyzed. TGAP/ND 1-5 system showed increase in modulus from 1676 to 3074 MPa, while greater modulus increase was seen for TGAP/MMT-ND 1-5 system in the range of 2388-3408 MPa. The balanced properties justified the application of novel epoxy nanocomposites in aviation industry.
       
  • Comparison of the Aerodynamic Characteristics of the NACA0012 Airfoil at
           Low-to-Moderate Reynolds Numbers for any Aspect Ratio

    • Abstract: Publication year: 2016Source: International Journal of Aerospace Sciences, Volume 4, Number 1S. Martínez-Aranda, A. L. García-González, L. Parras, J. F. Velázquez-Navarro, C. del PinoThis experimental work deals with the influence of the angle of attack (AoA) and the chord based Reynolds number (Rec) on the lift and drag coefficients for a low-aspect-ratio NACA0012 airfoil. In addition, we provide novel general correlations for the minimum drag coefficient together with the ratio between the maximum lift and the minimum drag coefficient for different Reynolds numbers and several aspect ratios, after comparing our experimental data with other research works. This information is very useful for future validation of numerical simulations. Furthermore, we observe that the change in the aerodynamic characteristics are linked to the variations in the linear slope of the lift coefficient as function of AoA for any aspect ratio, thus finding a critical Reynolds number Rec=105 at which the slope saturates its value and the maximum of the polar curve changes its upward trend.
       
  • Combustion Study of Composite Solid Propellants Containing Metal
           Phthalocyanines

    • Abstract: Publication year: 2014Source: International Journal of Aerospace Sciences, Volume 3, Number 2Lalith V. Kakumanu, Narendra Yadav, Srinibas KarmakarTransition metal Phthalocyanines have been used as burn rate modifiers for AP-HTPB composite solid propellants. An effort has been made to investigate the effect of Cu-Co-and Fe Phthalocyanines on the burn rate of composite propellants, as also on the combustion characteristics of such propellants. The burn rate has been determined in Crawford Strand Burner at 56 kg/cm2 pressure as also in low pressure burner setup at vacuum of 0.5 kg/cm2. Thermal analysis was performed using Thermo Gravimetric Analyzer (TGA), Differential Scanning Calorimeter (DSC) and heat of reaction has been measured by conventional Bomb Calorimeter. Scanning Electron Microscope (SEM) and Elemental Analyzer have been used for material characterization and possible composition of composite solid propellants. Metal Phthalocyanines have been found to influence the decomposition and to enhance the burn rate of the composite solid propellants.
       
 
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