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  Subjects -> AERONAUTICS AND SPACE FLIGHT (Total: 124 journals)
Showing 1 - 30 of 30 Journals sorted by number of followers
AIAA Journal     Hybrid Journal   (Followers: 1070)
SpaceNews     Free   (Followers: 820)
Journal of Spacecraft and Rockets     Hybrid Journal   (Followers: 735)
Journal of Propulsion and Power     Hybrid Journal   (Followers: 596)
Aviation Week     Full-text available via subscription   (Followers: 449)
Aerospace Science and Technology     Hybrid Journal   (Followers: 340)
IEEE Transactions on Aerospace and Electronic Systems     Hybrid Journal   (Followers: 330)
Advances in Space Research     Hybrid Journal   (Followers: 324)
IEEE Aerospace and Electronic Systems Magazine     Full-text available via subscription   (Followers: 290)
Journal of Aircraft     Hybrid Journal   (Followers: 288)
Control Systems     Hybrid Journal   (Followers: 259)
Acta Astronautica     Hybrid Journal   (Followers: 252)
Journal of Navigation     Hybrid Journal   (Followers: 215)
Gyroscopy and Navigation     Hybrid Journal   (Followers: 213)
Journal of Guidance, Control, and Dynamics     Hybrid Journal   (Followers: 211)
Aircraft Engineering and Aerospace Technology     Hybrid Journal   (Followers: 170)
Space Science International     Open Access   (Followers: 155)
Space Science Reviews     Hybrid Journal   (Followers: 92)
Propulsion and Power Research     Open Access   (Followers: 91)
International Journal of Aerospace Engineering     Open Access   (Followers: 83)
Progress in Aerospace Sciences     Full-text available via subscription   (Followers: 79)
Advances in Aerospace Engineering     Open Access   (Followers: 75)
Aerospace     Open Access   (Followers: 73)
Journal of Aerospace Engineering     Full-text available via subscription   (Followers: 60)
Journal of Aerospace Information Systems     Hybrid Journal   (Followers: 53)
Space Safety Magazine     Free   (Followers: 49)
International Journal of Aerodynamics     Hybrid Journal   (Followers: 47)
IEEE Transactions on Circuits and Systems I: Regular Papers     Hybrid Journal   (Followers: 46)
Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering     Hybrid Journal   (Followers: 42)
Space Research Today     Full-text available via subscription   (Followers: 42)
International Journal of Aeroacoustics     Hybrid Journal   (Followers: 36)
International Journal of Aerospace Sciences     Open Access   (Followers: 35)
Journal of Aeronautics & Aerospace Engineering     Open Access   (Followers: 31)
Aviation Psychology and Applied Human Factors     Hybrid Journal   (Followers: 30)
Journal of Aerodynamics     Open Access   (Followers: 30)
Space Policy     Hybrid Journal   (Followers: 29)
Canadian Aeronautics and Space Journal     Full-text available via subscription   (Followers: 29)
CEAS Aeronautical Journal     Hybrid Journal   (Followers: 29)
Egyptian Journal of Remote Sensing and Space Science     Open Access   (Followers: 29)
Journal of Space Weather and Space Climate     Open Access   (Followers: 29)
Aerospace Medicine and Human Performance     Full-text available via subscription   (Followers: 27)
Journal of Wind Engineering and Industrial Aerodynamics     Hybrid Journal   (Followers: 26)
International Journal of Aerospace Innovations     Full-text available via subscription   (Followers: 26)
Journal of Aerospace Information Systems     Hybrid Journal   (Followers: 25)
Nonlinear Dynamics     Hybrid Journal   (Followers: 24)
Russian Aeronautics (Iz VUZ)     Hybrid Journal   (Followers: 24)
International Journal of Aerospace Psychology     Hybrid Journal   (Followers: 22)
Frontiers in Aerospace Engineering     Open Access   (Followers: 22)
Artificial Satellites     Open Access   (Followers: 21)
Chinese Journal of Aeronautics     Open Access   (Followers: 20)
Journal of Aerospace Engineering & Technology     Full-text available via subscription   (Followers: 20)
Proceedings of the Human Factors and Ergonomics Society Annual Meeting     Hybrid Journal   (Followers: 20)
International Journal of Space Structures     Full-text available via subscription   (Followers: 19)
International Journal of Satellite Communications Policy and Management     Hybrid Journal   (Followers: 18)
Fatigue of Aircraft Structures     Open Access   (Followers: 17)
Research & Reviews : Journal of Space Science & Technology     Full-text available via subscription   (Followers: 17)
Advances in Aerospace Science and Technology     Open Access   (Followers: 17)
Frontiers in Astronomy and Space Sciences     Open Access   (Followers: 15)
Aeronautical Journal, The     Hybrid Journal   (Followers: 14)
Aviation     Open Access   (Followers: 12)
Journal of Airline and Airport Management     Open Access   (Followers: 12)
Journal of Aviation Technology and Engineering     Open Access   (Followers: 12)
Journal of the Astronautical Sciences     Hybrid Journal   (Followers: 12)
Journal of Aircraft and Spacecraft Technology     Open Access   (Followers: 12)
International Journal of Crashworthiness     Hybrid Journal   (Followers: 11)
International Journal of Micro Air Vehicles     Open Access   (Followers: 11)
International Journal of Space Technology Management and Innovation     Full-text available via subscription   (Followers: 11)
Aerospace Systems     Hybrid Journal   (Followers: 11)
Population Space and Place     Hybrid Journal   (Followers: 10)
Journal of the American Helicopter Society     Full-text available via subscription   (Followers: 10)
International Journal of Space Science and Engineering     Hybrid Journal   (Followers: 10)
Air Force Magazine     Full-text available via subscription   (Followers: 10)
Journal of Aerospace Technology and Management     Open Access   (Followers: 10)
Journal of Aeronautical Materials     Open Access   (Followers: 9)
International Journal of Applied Geospatial Research     Hybrid Journal   (Followers: 8)
Journal of Space Safety Engineering     Hybrid Journal   (Followers: 8)
International Journal of Aviation, Aeronautics, and Aerospace     Open Access   (Followers: 8)
Aerotecnica Missili & Spazio : Journal of Aerospace Science, Technologies & Systems     Hybrid Journal   (Followers: 8)
Transportmetrica A : Transport Science     Hybrid Journal   (Followers: 7)
International Journal of Aviation Technology, Engineering and Management     Full-text available via subscription   (Followers: 7)
Aerospace technic and technology     Open Access   (Followers: 7)
Air Medical Journal     Hybrid Journal   (Followers: 6)
Space and Polity     Hybrid Journal   (Followers: 6)
International Journal of Aviation Management     Hybrid Journal   (Followers: 6)
Aviation in Focus - Journal of Aeronautical Sciences     Open Access   (Followers: 6)
New Space     Hybrid Journal   (Followers: 6)
Journal of Astrobiology & Outreach     Open Access   (Followers: 6)
RocketSTEM     Free   (Followers: 6)
Civil Aviation High Technologies     Open Access   (Followers: 6)
Cosmic Research     Hybrid Journal   (Followers: 5)
International Journal of Sustainable Aviation     Hybrid Journal   (Followers: 5)
Transport and Aerospace Engineering     Open Access   (Followers: 5)
Life Sciences in Space Research     Hybrid Journal   (Followers: 5)
International Journal of Aeronautical and Space Sciences     Hybrid Journal   (Followers: 5)
Journal of Spatial Science     Hybrid Journal   (Followers: 4)
Journal of KONBiN     Open Access   (Followers: 4)
Unmanned Systems     Hybrid Journal   (Followers: 4)
REACH - Reviews in Human Space Exploration     Full-text available via subscription   (Followers: 4)
Astrodynamics     Hybrid Journal   (Followers: 4)
Advances in Astronautics Science and Technology     Hybrid Journal   (Followers: 4)
IEEE Journal on Miniaturization for Air and Space Systems     Hybrid Journal   (Followers: 4)
Perspectives of Earth and Space Scientists i     Open Access   (Followers: 4)
Microgravity Science and Technology     Hybrid Journal   (Followers: 3)
ASTRA Proceedings     Open Access   (Followers: 3)
npj Microgravity     Open Access   (Followers: 3)
Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa / Problems of Mechatronics. Armament, Aviation, Safety Engineering     Open Access   (Followers: 3)
Ciencia y Poder Aéreo     Open Access   (Followers: 3)
Open Aerospace Engineering Journal     Open Access   (Followers: 3)
Journal of Engineering and Technological Sciences     Open Access   (Followers: 2)
MAD - Magazine of Aviation Development     Open Access   (Followers: 2)
Journal of Aviation/Aerospace Education & Research     Open Access   (Followers: 2)
Investigación Pecuaria     Open Access   (Followers: 2)
Transactions on Aerospace Research     Open Access   (Followers: 2)
Вісник Національного Авіаційного Університету     Open Access   (Followers: 1)
Science and Education : Scientific Publication of BMSTU     Open Access   (Followers: 1)
Spatial Information Research     Hybrid Journal   (Followers: 1)
Journal of the Australasian Society of Aerospace Medicine     Open Access   (Followers: 1)
Mekanika : Jurnal Teknik Mesin i     Open Access   (Followers: 1)
Xibei Gongye Daxue Xuebao / Journal of Northwestern Polytechnical University     Open Access   (Followers: 1)

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Similar Journals
Journal Cover
Journal of Aerodynamics
Number of Followers: 30  

  This is an Open Access Journal Open Access journal
ISSN (Print) 2356-7139 - ISSN (Online) 2314-6206
Published by Hindawi Homepage  [340 journals]
  • Impact of Surface Roughness on the Turbulent Wake Flow of a Turbine Blade

    • Abstract: Roughened aeroengine blade surfaces lead to increased friction losses and reduced efficiency of the individual blades. The surface roughness also affects the wake flow of the blade and thus the inflow conditions for the subsequent compressor or turbine stage. To investigate the impact of surface roughness on a turbulent blade wake, we conducted velocity field measurements by means of stereo particle image velocimetry in the wake of a roughened turbine blade in a linear cascade wind tunnel. The turbine blade was roughened at different chordwise locations. The influence of the chordwise location of the added surface roughness was examined by comparing their impact on the width and depth of the wake and, the positions and distribution of vortical structures in the wake. Additionally, the friction loss coefficients for different surface roughness positions were estimated directly from the velocity field.
      PubDate: Tue, 30 Dec 2014 11:58:26 +000
  • Shape Optimization of an Airfoil in Ground Effect for Application to WIG

    • Abstract: This paper employs a multiobjective genetic algorithm (MOGA) to optimize the shape of a widely used wing in ground (WIG) aircraft airfoil NACA 4412 to improve its lift and drag characteristics, in particular to achieve two objectives, that is, to increase its lift and its lift to drag ratio. The commercial software ANSYS FLUENT is employed to calculate the flow field on an adaptive structured mesh generated by ANSYS ICEM software using the Reynolds-Averaged Navier-Stokes (RANS) equations in conjunction with a one equation Spalart-Allmaras (SA) turbulence model. The results show significant improvement in both the lift coefficient and lift to drag ratio of the optimized airfoil compared to the original NACA 4412 airfoil. It is demonstrated that the performance of a wing in ground (WIG) aircraft can be improved by using the optimized airfoil.
      PubDate: Mon, 08 Dec 2014 08:09:28 +000
  • Computational Aerodynamic Analysis of Offshore Upwind and Downwind

    • Abstract: Aerodynamic interactions of the model NREL 5 MW offshore horizontal axis wind turbines (HAWT) are investigated using a high-fidelity computational fluid dynamics (CFD) analysis. Four wind turbine configurations are considered; three-bladed upwind and downwind and two-bladed upwind and downwind configurations, which operate at two different rotor speeds of 12.1 and 16 RPM. In the present study, both steady and unsteady aerodynamic loads, such as the rotor torque, blade hub bending moment, and base the tower bending moment of the tower, are evaluated in detail to provide overall assessment of different wind turbine configurations. Aerodynamic interactions between the rotor and tower are analyzed, including the rotor wake development downstream. The computational analysis provides insight into aerodynamic performance of the upwind and downwind, two- and three-bladed horizontal axis wind turbines.
      PubDate: Wed, 29 Oct 2014 09:10:24 +000
  • Wind Loads of Solar Water Heaters: Wind Incidence Effect

    • Abstract: For applications of solar thermal energy, solar water heaters (SWHs) are becoming common. In this study, the effect of a crosswind on the aerodynamic characteristics of residential (an inclined flat plate with a horizontal cylinder) and large-scale SWHs (an inclined flat plate only) is experimentally investigated. The tests are conducted in a low speed wind tunnel and the relative wind direction with respect to the test model, , ranges from 0 to 135 deg. Measurements of the mean and fluctuating pressures are presented. These results demonstrate that higher suction and fluctuating pressure are observed near the upwind corner, particularly for the test case of  deg.
      PubDate: Mon, 27 Oct 2014 13:11:57 +000
  • On the Kutta Condition in Potential Flow over Airfoil

    • Abstract: This paper proposes a novel method to implement the Kutta condition in irrotational, inviscid, incompressible flow (potential flow) over an airfoil. In contrast to common practice, this method is not based on the panel method. It is based on a finite difference scheme formulated on a boundary-fitted grid using an O-type elliptic grid generation technique. The proposed algorithm uses a novel and fast procedure to implement the Kutta condition by calculating the stream function over the airfoil surface through the derived expression for the airfoils with both finite trailing edge angle and cusped trailing edge. The results obtained show the excellent agreement with the results from analytical and panel methods thereby confirming the accuracy and correctness of the proposed method.
      PubDate: Tue, 01 Apr 2014 08:17:19 +000
  • Drag Reduction of Passenger Car Using Add-On Devices

    • Abstract: This work proposes an effective numerical model using the Computational Fluid Dynamics (CFD) to obtain the flow structure around a passenger car with different add-on devices. The computational/numerical model of the passenger car and mesh was constructed using ANSYS Fluent which is the CFD solver and employed in the present work. In this study, numerical iterations are completed, and then aerodynamic data and detailed complicated flow structure are visualized. In the present work, a model of generic passenger car was developed using solidworks, generated the wind tunnel, and applied the boundary conditions in ANSYS workbench platform, and then testing and simulation have been performed for the evaluation of drag coefficient for passenger car. In another case, the aerodynamics of the most suitable design of vortex generator, spoiler, tail plates, and spoiler with VGs are introduced and analysed for the evaluation of drag coefficient for passenger car. The addition of these add-on devices are reduces the drag-coefficient and lift coefficient in head-on wind. Rounding the edges partially reduces drag in head-on wind but does not bring about the significant improvements in the aerodynamic efficiency of the passenger car with add-on devices, and it can be obtained. Hence, the drag force can be reduced by using add-on devices on vehicle and fuel economy, stability of a passenger car can be improved.
      PubDate: Sun, 23 Mar 2014 07:54:48 +000
  • Calibration Technique for Recovery of Short Duration Aerodynamic Force

    • Abstract: Force measurement is one of the key issues for design of high speed vehicle configurations. They are routinely tested in impulse facilities where the test duration is in the order of few milliseconds. Since, the experiments are performed in short test times, it is expected that the model never achieves the steady state. So, the measurement diagnostics must account this fact while inferring the forces from the measured parameters. One of the methods is the determination of characteristics system response function by including the dynamics of the system. The aim of this work is to develop a calibration experimental setup and measure axial force on generic aerodynamic body configurations during a short time (~0.6 ms). A generic aerodynamic model attached to a “stress bar” is suspended freely and an impulse load is applied at the tip of the model. An accelerometer fitted with the model records the signal corresponding to the motion of the model. Then, the system characteristics function (impulse response function) is obtained from input force history and output accelerometer signal and further used to predict any unknown forces of similar nature. The recovered forces are compared well with the applied ones with a reasonable accuracy of %.
      PubDate: Tue, 04 Mar 2014 12:32:24 +000
  • Experimental Evaluation of an Internally Passively Pressurized Circulation
           Control Propeller

    • Abstract: The purpose of circulation control for fixed wing aircrafts is to increase the lifting force when large lifting forces and/or slow speeds are required, such as at takeoff and landing. Wing flaps and slats are used on almost all fixed-wing aircraft. While effective in increasing lift, they do so with penalty of increasing drag, weight, and control complexity. The goal of this research was to find an alternative way of pumping pressurized air to the trailing edge slot on a UAV propeller. This design called for rerouting stagnation pressure from the frontal propeller area through the inside of the propeller blades to ejection slots on the trailing edge. This allows for the forward velocity of the aircraft to drive the pressurization of the circulation control plenum passively, without additional hardware. For this study, a Clark-Y airfoil section propeller with an overall diameter of 0.609 meters was designed and tested. The comparison of the augmented to unaugmented propeller showed a 5.12 percent increase in efficiency, which is shown to act over the entire range of flight envelopes of the aircraft and is shown to be particularly beneficial at advance ratios above 0.30, normal operating conditions of propeller-driven UAVs.
      PubDate: Mon, 03 Feb 2014 08:39:50 +000
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