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    Investigation of a new flux scheme for the numerical simulation of the supersonic intake flow

    Soltani, M R / Younsi, J S / Farahani, M | SAGE Publications | 2012
    A numerical code for supersonic intake design with a proper simulation of the normal and/or oblique shocks, boundary layer development ...

    Effect of optimal slot location on the performance of cascades of blades

    Bakhtiari Nia, Bahador / Gharehghani, Ayat / Shojae Zadeh, Saeed et al. | SAGE Publications | 2021
    potential method to stand against the boundary layer separation for this issue. In the present study, the different locations of passive flow ...
    Schlagwörter: cascade of compressor blades

    Effect of flexion on the propulsive performance of a flexible flapping wing

    Deng, Shuanghou / Xiao, Tianhang | SAGE Publications | 2016
    A numerical study was carried out to investigate the effect of chordwise flexion on the propulsive performance of a two-dimensional ...

    Effect of air jet with injection pressure on the performance of mixed compression air intake

    Gahlot, NK / Singh, NK | SAGE Publications | 2021
    A computational study on the performance of mixed compression supersonic air intake has been carried out with and without air jet at ...

    Effect of geometric parameters on the spray cone angle in the pressure swirl injector

    Liu, Juan / Zhang, Xin-Qiao / Li, Qing-Lian et al. | SAGE Publications | 2013
    Spray cone angle affects the droplet distribution after atomization and is one of the main targets of coaxial gas–liquid injector ...

    An optimal design model for the wall thickness of the propellant tank

    Xin, Tengda / Wang, Hua / Cui, Cunyan et al. | SAGE Publications | 2020
    The propellant tank is a vital part for the liquid rocket, and the optimal design of the propellant tank is a significant research to ...

    Effects of strut swept angle on the drag of scramjet

    Bao, W / Zong, Y / Chang, J et al. | SAGE Publications | 2012
    Swept angle is one of the most important geometric parameters of the strut in scramjet. The change in swept angle will make the geometric ...

    Experimental study of riblet effects on the aerodynamic performance and flow characteristics of a delta wing

    Saeedi Rizi, Behnam / Nili-Ahmadabadi, Mahdi / Nafar Sefiddashti, Mehrdad et al. | SAGE Publications | 2019
    The present study investigates the effects of riblet on the aerodynamic performance and flow characteristics of a delta wing. Flow ...

    Determination of the flight trajectory in terms of emission and fuel consumption minimization

    Pawlak, Małgorzata / Kuźniar, Michał / Majka, Andrzej R. | SAGE Publications | 2022
    The present-day world is characterized by the intense development of air transport. However, along with it, significant problems appear ...

    Mechanism of affecting the axial rotor stability and performance with center offset degrees of axial skewed slots

    Zhang, HaoGuang / Wang, Enhao / Liu, WenHao et al. | SAGE Publications | 2020
    the effects of the center offset degree (Cod) on the rotor stability and performance. Cod is defined as the ratio of the central difference ...

    Identifying pitching mode of aerial planting projectile by the use of image processing

    Goodarzi, H / Sabzehparvar, M | SAGE Publications | 2017
    dynamics of an aerial planting projectile has been simulated using data of the wind tunnel test. By creating the projectile graphical model and ...

    The effect of representative bird model and its impact direction on crashworthiness of aircraft windshield and canopy structure

    Dar, Uzair A / Awais, Muhammad / Mian, Haris H et al. | SAGE Publications | 2019
    give better representation of a real bird, in this study, the bird was modeled as a fluid body while impacting the rigid and deformable ...

    Impact of biofuel blends on the emissions of modern vehicles

    Pelkmans, L / Lenaers, G / Bruyninx, J et al. | SAGE Publications | 2011
    of the test results. ...

    Influence of key geometric parameters on the aerodynamic performance of a supersonic compressor cascade

    Cui, Cui / Zhou, Zhenggui / Zhang, Jinhuan et al. | SAGE Publications | 2018
    of the leading-edge radius, cascade solidity, and pre-compression on the aerodynamic performance of a supersonic cascade. The cascade is ...

    The effect of edge profile on delta wing flow

    Mat, Shabudin Bin / Green, Richard / Galbraith, Roderick et al. | SAGE Publications | 2016
    -edged, small, medium, and large radius. The experiments were performed as a part of the European Vortex Flow Experiment-2 campaign. Tests were ...
    Schlagwörter: angle of attack

    Effect of temperature on the dynamic performance of C/C composite finger seal

    Wang, Li-Na / Chen, Guo-Ding / Su, Hua et al. | SAGE Publications | 2016
    The designs of sealing device have prominent influence on the performance of aero-engine. The high temperature environment during the ...

    Effect of spanwise groove on the dynamic stall characteristics of an airfoil

    Yadav, Rajesh / Bodavula, Aslesha | SAGE Publications | 2022
    Numerical simulations are conducted to investigate the effect of triangular groove on the dynamic stall characteristics of a NACA 0012 ...

    Numerical and experimental investigation of the mean and turbulent characteristics of a wing-tip vortex in the near field

    O’Regan, Micheál S / Griffin, Philip C / Young, Trevor M | SAGE Publications | 2014
    The near-field (up to three chord lengths) development of a wing-tip vortex is investigated both numerically and experimentally. The ...

    Metamodel-based optimization of the bolted connection of a wing spar considering fatigue resistance

    Xia, Tianxiang / Yao, Weixing / Xu, Lipu et al. | SAGE Publications | 2016
    In this paper, the optimization considering the constraint of fatigue life was conducted on a bolted connection of a wing spar, after which ...

    The effect of a tandem vane crossover diffuser configuration on the performance of a MGT mixed flow compressor

    Freier Zugriff
    van Eck, Hano / van der Spuy, Sybrand Johannes | SAGE Publications | 2024

    Due to the inherent geometric restrictions of a micro gas turbine (MGT) mixed flow compressor design, diffuser design has a major impact

     ...

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