1–20 von 26 Ergebnissen
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    Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop

    Murayama, M. / Yamamoto, K. / Ito, Y. et al. | British Library Conference Proceedings | 2015

    CFD COMPARISON STUDY FOR TRAPEZOIDAL HIGH-LIFT WING CONFIGURATIONS BY STRUCTURED AND UNSTRUCTURED MESH METHOD

    Murayama, M. / Yamamoto, K. / Tanaka, K. et al. | British Library Conference Proceedings | 2011

    Comparison Study of Drag Prediction for the 4th CFD Drag Prediction Workshop Using a Structured and an Unstructured Mesh Methods

    Yamamoto, K. / Tanaka, K. / Murayama, M. et al. | British Library Conference Proceedings | 2010

    Computational Studies of the NASA High-Lift Trap Wing Using Structured and Unstructured Grid Solvers

    Murayama, M. / Yamamoto, K. / Ito, Y. et al. | British Library Conference Proceedings | 2012

    Summary of JAXA Studies for the Second AIAA CFD High Lift Prediction Workshop Using Structured and Unstructured Mesh CFD (AIAA 2014-2396)

    Murayama, M. / Yamamoto, K. / Ito, Y. et al. | British Library Conference Proceedings | 2014

    High-Quality Unstructured Hybrid Mesh Generation for Capturing Effects of Vortex Generators

    Ito, Y. / Murayama, M. / Yamamoto, K. et al. | British Library Conference Proceedings | 2013

    Turbulent Flow Solver Validation of FaSTAR and UPACS (AIAA 2014-0240)

    Hashimoto, A. / Murayama, M. / Yamamoto, K. et al. | British Library Conference Proceedings | 2014

    Validation of Flows on High-Lift Configurations by Structured- and Unstructured- Mesh Method

    Murayama, M. / Yamamoto, K. / Kobayashi, K. et al. | British Library Conference Proceedings | 2005

    Comparison Study of Drag Prediction for the 3rd CFD Drag Prediction Workshop by Structured and Unstructured Mesh Method (Invited) AIAA Paper

    Murayama, M. / Yamamoto, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    AIAA 2006-1396 Comparison of RANS Simulations of Multi-Element High-Lift Configurations

    Murayama, M. / Imamura, T. / Yamamoto, K. et al. | British Library Conference Proceedings | 2006

    Aeroacoustic Simulation of JAXA Landing Gear by Building-Cube Method and Non-Compact Curle's Equation

    Deguchi, A. / Sasaki, D. / Nakahashi, K. et al. | British Library Conference Proceedings | 2012

    Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel

    Murayama, M. / Yokokawa, Y. / Tanaka, K. et al. | British Library Conference Proceedings | 2008

    DRAG PREDICTION ON NASA CRM USING AUTOMATIC HEXAHEDRA GRID GENERATION

    Hashimoto, A. / Murakami, K. / Aoyama, T. et al. | British Library Conference Proceedings | 2010

    AERODYNAMIC INFLUENCE OF A HALF-SPAN MODEL INSTALLATION FOR HIGH-LIFT CONFIGURATION EXPERIMENT

    Yokokawa, Y. / Murayama, M. / Uchida, H. et al. | British Library Conference Proceedings | 2010

    Summary of JAXA Studies for the Fifth AIAA CFD Drag Prediction Workshop Using UPACS and FaSTAR

    Murayama, M. / Yamamoto, K. / Hashimoto, A. et al. | British Library Conference Proceedings | 2013

    EFFICIENT OPTIMIZATION DESIGN METHOD USING KRIGING MODEL

    Jeong, S. / Murayama, M. / Yamamoto, K. et al. | British Library Conference Proceedings | 2004

    Investigation and Improvement of High-Lift Aerodynamic Performances in Lowspeed Wind Tunnel Testing

    Yokokawa, Y. / Murayama, M. / Kanazaki, M. et al. | British Library Conference Proceedings | 2008

    CFD Validation Study for a High-Lift Configuration of a Civil Aircraft Model

    Murayama, M. / Yokokawa, Y. / Yamamoto, K. et al. | British Library Conference Proceedings | 2007

    Experiment and CFD of a High-Lift Configuration Civil Transport Aircraft Model

    Yokokawa, Y. / Murayama, M. / Ito, T. et al. | British Library Conference Proceedings | 2006