1–20 von 420 Ergebnissen
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    Large-Eddy Simulation of Aircraft Wake Vortex Deformation and Topology

    Freier Zugriff
    Hennemann, Ingo / Holzäpfel, Frank | Deutsches Zentrum für Luft- und Raumfahrt (DLR) | 2011

      Large-eddy simulation of aircraft wake vortex deformation and topology

      Hennemann, I. / Holzäpfel, F. | Tema Archiv | 2011

    Numerical Calculation of Effect of Elastic Deformation on Aerodynamic Characteristics of a Rocket

    Abbas, Laith K. / Chen, Dongyang / Rui, Xiaoting et al. | Tema Archiv | 2014

    FE Analysis of Dynamic Response of Aircraft Windshield against Bird Impact

    Dar, Uzair Ahmed / Zhang, Weihong / Xu, Yingjie et al. | Tema Archiv | 2013

    Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter

    Caliskan, Fikret / Zhang, Youmin / Wu, N. Eva et al. | Tema Archiv | 2014

    An Efficient Nonlinear Filter for Spacecraft Attitude Estimation

    Liu, Bing / Chen, Zhen / Liu, Xiangdong et al. | Tema Archiv | 2014

    Relative Navigation in LEO by Carrier-Phase Differential GPS with Intersatellite Ranging Augmentation

    Renga, Alfredo / Grassi, Michele / Tancredi, Urbano et al. | Tema Archiv | 2013

    Boost Full Bridge Bidirectional DC/DC Converter for Supervised Aeronautical Applications

    Cavallo, Alberto / Guida, Beniamino / Rubino, Luigi et al. | Tema Archiv | 2014

    Helicopter Vibratory Loads Alleviation through Combined Action of Trailing-Edge Flap and Variable-Stiffness Devices

    Gennaretti, Massimo / Bernardini, Giovanni / Serafini, Jacopo et al. | Tema Archiv | 2015

    Adaptive and Resilient Flight Control System for a Small Unmanned Aerial System

    Garcia, Gonzalo / Keshmiri, Shahriar / Avdelidis, Nicolas | Tema Archiv | 2013

    Real-Time Hardware-in-the-Loop Laboratory Testing for Multisensor Sense and Avoid Systems

    Fasano, Giancarmine / Accardo, Domenico / Forlenza, Lidia et al. | Tema Archiv | 2013

    Airloads Correlation of the UH-60A Rotor inside the 40- by 80-Foot Wind Tunnel

    Chang, I.Chung / Norman, Thomas R. / Romander, Ethan A. et al. | Tema Archiv | 2014

    A New Method for Initial Parameters Optimization of Guided Projectiles

    Feng, Bi-Ming / Nie, Wan-Sheng / Ganguli, R. | Tema Archiv | 2013

    Model-based fault diagnosis for aerospace systems: A survey

    Marzat, J. / Piet-Lahanier, H. / Damongeot, F. et al. | Tema Archiv | 2012

    A new method for design of fixed wing micro air vehicle

    Hassanalian, Mostafa / Khaki, Hamed / Khosravi, Mehrdad | Tema Archiv | 2015

    Experimental study on the lift generated by a flapping rotary wing applied in a micro air vehicle

    Zhou, Chao / Wu, Jianghao / Guo, Shijun et al. | Tema Archiv | 2014

    A new pipe routing method for aero-engines based on genetic algorithm

    Ren, Tao / Zhu, Zhi-liang / Dimirovski, Georgi M. et al. | Tema Archiv | 2014

    Body under lifting wing

    Chen, C.F. / Clarke, J.H. | Engineering Index Backfile | 1961

    Supersonic boom of wing-body configurations

    Ryhming, I.L. / Yoler, Y.A. | Engineering Index Backfile | 1961