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title: aerospace actuator 1

Synonyme wurden verwendet für: Actuators
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    Achieving a High-Speed and Momentum Synthetic Jet Actuator

    Amitay, Michael | Online Contents | 2016
    momentum synthetic jet, with a peak velocity exceeding 200  m/s. A total of two scales of actuator apparatuses having either 40- or 80-mm-diameter ...
    Schlagwörter: Actuators

    Achieving a High-Speed and Momentum Synthetic Jet Actuator

    Van Buren, Tyler / Whalen, Edward / Amitay, Michael | ASCE | 2015
    200     m / s . A total of two scales of actuator ...

    Gurney-Flap Drag Penalty Reduction with a DBD Plasma Actuator

    Zhang, Zeng / Feng, Lihao / Wang, Jinjun et al. | ASCE | 2017
    (DBD) plasma actuator, which was mounted in front of the Gurney flap to generate a countercurrent wall jet. The research was based on numerical ...

      Gurney-Flap Drag Penalty Reduction with a DBD Plasma Actuator

      Zhang, Zeng | Online Contents | 2017
      actuator, which was mounted in front of the Gurney flap to generate a countercurrent wall jet. The research was based on numerical simulation ...
      Schlagwörter: Actuators

    L1 Adaptive Control of a Projectile Fin by Piezoelectric Actuator

    Lee, Keum W. / Singh, Sahjendra N. | ASCE | 2012
    1 adaptive control system is designed for the control of a projectile fin. The rotational ...

    Separated-Flow Control Simulation with a Periodic Excitation by SDBD Plasma Actuator at Re=O(205)

    Bernal-Orozco, R. A. / Arias-Montano, Alfredo / Huerta-Chávez, O. | ASCE | 2020
    dielectric-barrier discharge (SDBD) plasma actuator applied to an airfoil section at ...

    Bombardier Global 7500 Fatigue Test Cycle Rate Commissioning to ¼ Life

    André Beltempo, C. / Beaudoin, Alexandre / Pothier, Robert | Springer Verlag | 2019
    and damage tolerance test (DADTT), as conducted by the experimental department of Bombardier Aerospace (BAEX). A rapid test rig commissioning ...
    Schlagwörter: Aerospace Technology and Astronautics

    Numerical Investigation on Flow Control of a Hypersonic Airfoil by Plasma Synthetic Jet

    Sun, Zhikun / Shi, Zhiwei / Zhang, Weilin et al. | ASCE | 2022
    study found that the geometric position of a PSJ actuator on an airfoil surface is the key factor affecting flow control effects. Different ...

    Post-buckled precompressed techniques in adaptive aerostructures: An overview

    Vos, Roelof / Barrett, Ron | Tema Archiv | 2009
    the actuator element. In doing so the mechanical work output has been shown to increase three-fold compared to conventional bimorph actuators ...
    Schlagwörter: piezoelektrischer Aktor , piezoelektrischer PBP-Aktor (post-buckled precompressed)

    Control of structural flutter using piezoelectric patches

    Hariri, M. / John, S. / Trivallo, P. | Tema Archiv | 2009
    Aero-elasticity is a major concern in aerospace field. It resultes from the interaction between the air-stream and the structure. Wing ...
    Schlagwörter: piezoelektrischer Aktor

    Characterization of Epoxy Resin Including Strain Rate Effects Using Digital Image Correlation System

    Fard, Masoud Yekani / Liu, Yingtao / Chattopadhyay, Aditi | ASCE | 2011
    0.03     s - 1 . Two types of dog ...

    Experimental Investigation of Flow Control on a High-Lift Wing Using Modulated Pulse Jet Vortex Generator

    Abdolahipour, Soheila / Mani, Mahmoud / Shams Taleghani, Arash | ASCE | 2022
    were used as actuators to excite the flow. The vortex generator slot pairs were incorporated into the shoulder of the trailing-edge flap, where ...

    Airfoil morphing architecture based on shape memory alloys

    Barbarino, Silvestro / Pecora, Rosario / Lecce, Leonardo et al. | Tema Archiv | 2009
    these critical tasks. The so-called Smart Structure idea is more and more taken into account in aerospace applications. Among the family of ...
    Schlagwörter: Aktor

    Overview of Boeing's shape memory alloy based morphing aerostructure

    Calkins, F.T. / Mabe, J.H. / Ruggeri, R.T. | Tema Archiv | 2009
    -Nitinol tube actuators to twist a rotor blade in a spin stand test to optimize aerodynamic characteristics. The Variable Geometry Chevrons program ...
    Schlagwörter: Aktor

    Novel load-introduction systems for lightweight aircraft components in composite-metal-hybrid design

    Hufenbach, W. / Gude, M. / Helms, O. et al. | Tema Archiv | 2008
    The ever increasing competition forces the aerospace industry to reduce the weight of aircrafts which leads to an increased payload and ...

    Robustness of velocity feedback controllers for flexible spacecraft

    Joshi, S.M. | Tema Archiv | 1985
    structures are investigated. It is proved that the closed-loop system using such controllers is asymptotically stable when: (1) unmodeled linear time ...
    Schlagwörter: AEROSPACE CONTROL

    Engineers refine high-pressure systems

    Tema Archiv | 1989
    einer Leistung von 151 1/min, die der Abex Aerospace lief bereits 500 hr. Neue Metall-Metall-Leitungsverbinder mit Silicondichtung sind aus ...

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