References
- Yu XiongQing, Xu HuiMin, and Ang HaiSong. Aircraft conceptual/preliminary design. Beijing: Aviation Industry Press, 2000, Chinese.
- Raymer D P., Aircraft design: a conceptual approach. 3rd Edition, Reston: AIAA Inc, 1999.
- Gu Songfen, and Xie Sishi., Aircraft conceptual/preliminary design, Beijing: BeiHang University Press, 2001, Chinese.
- Li W J., Aircraft conceptual/preliminary design, Xian: Northwestern Polytechnical University Press, 2005, Chinese.
- Jan Roskam., Aircraft Design, Roskam Aviation and Engineering Corporation, 1985.
- Ajoy Kundu., Aircraft Design, Cambridge: Cambridge University Press, 2010.
- Bindolino G, Ghiringhelli G, and Ricci S, et al. "Multilevel structural optimization for preliminary wing-box weight estimation", Journal of Aircraft, Vol. 47, No.2, 2010, pp. 475-489. https://doi.org/10.2514/1.41552
- Ma J X., "Weight Prediction Technology Based on Modeling and Multidisciplinary Analysis", Journal of Aeronautical Manufacturing Technology, Vol. ?, No.7, 2012, pp. 26-30.
- Ledermann C, Ermanni P, and Kelm R. "Dynamic CAD objects for structural optimization in preliminary aircraft design", Journal of Aerospace science and technology, Vol. 10, No. 7, 2006, pp. 601-610. https://doi.org/10.1016/j.ast.2006.07.001
- Elham A, La Rocca G, and van Tooren M J L., "Development and implementation of an advanced, designsensitive method for wing weight estimation", Aerospace Science and Technology, Vol. 29, No. 1, 2013, pp. 100-113. https://doi.org/10.1016/j.ast.2013.01.012
- Wei Si., Weight Estimation of Wings in Preliminary Aircraft Design[D], Nanjing University of Aeronautics and Astronautics, 2010, Chinese.
- M. Droegkamp., Finite element model weight estimation, SAWE Paper No. 2089, May 1992.
- G. Bindolino, G. Ghiringhelli, S. Ricci, and M. Terraneo., "Multilevel structural opti-mization for preliminary wing-box weight estimation", Journal of Aircraft, Vol. 47, No. 2, 2010, pp. 475-489. https://doi.org/10.2514/1.41552
- M. Laban, P. Arendsen, W. Rouwhorst, and W. Vankan, "A computational design engine for multidisciplinary optimisation with application to a blended wing body configuration", AIAA Paper 91-5058, in: 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimisation, Atlanta, 2002.
- F. Hurlimann, R. Kelm, M. Dugas, K. Oltmann, and G. Kress, "Mass estimation of transport aircraft wingbox structures with a CAD/CAE-based multidisciplinary process", Aerospace Science and Technology, Vol. 15, No. 4, 2011, pp. 323-333. https://doi.org/10.1016/j.ast.2010.08.005
- M. Sensmeier, B. Stewart, and amareh, "Rapid generation and assessment of aircraft structural topologies for multidisciplinary optimization and weight estimation", in: Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Vol. 7, 2006, pp. 4722-4733.
- Wang G L, Sun Y D, and Wu Z., "Rapid uniform aliform component modeling based on parameter in conceptual aircraft design", Acts Aeronautics et Astronautics Sinica, Vol. 23, No. 6, 2002, pp. 575-578.
- Luo Mingqiang, Feng Haocheng, Liu Hu and Wu Zhe., "Rapid wing structure design and automated scheme adjustment for civil aircraft", Journal of Beijing University of Aeronautics and Astronautics, Vol. 4:0.18, 2009.
- Luo Mingqiang, Feng Haocheng, Liu Hu and Wu Zhe., "Rapid wing structural finite element modeling and automated adjustment". Journal of Beijing University of Aeronautics and Astronautics, Vol. 6:0.12, 2011.
- Luo Mingqiang, Wei Chenglong, Liu Hu and Wu Zhe., "Rapid Estimation Method for Aircraft Weight and Center of Gravity Based on 3-D Parametric Modeling", Acta Aeronautica ET Astronautica Sinica, Vol. 34, No. 3, 2013, pp. 566-573.
- Li ZhengNeng, Zhang YuZhu, Fang WeiGuo., Aircraft Structure. Beijing: BeiHang University Press, 2005, Chinese.
- Roberts R W, Canfield R A, and Blair M., "Sensor-craft structural optimization and analytical certification", AIAA-2005-1458, 2005.
- Choi S, Alonso J J, and Kroo I ,M., "Multifidelity Design Optimization of Low-Boom Supersonic Jets", Journal of Aircraft. Vol. 45:1, 2008.
- Taira T, Jeong S, and Obayashi S, et al., "GUI-based Geometry Deformation Tool for Modification of Aircraft Configurations[C]", 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013.
- Thomas J L and Miller D S., "Numerical Comparisons of Panel Methods at Subsonic and Supersonic Speeds", AIAA paper, 79-0404, January 1979.
- Sytsma H S, Hewill B L and Rubbert P E., "A Comparison of Panel Methods for Subsonic Flow. Computation", AGARD Paper 241, May 1976.
- Thomas J L, Luckring J M, and Sellers M W L., "Evaluation of Factors Determining the Accuracy of Linearized Subsonic Panel Methods", AIAA 83-1826.
- Tinoco E N, Ball D N and Rice F A., "PAN AIR Analysis of a Transport High-Lift Configuration. Journal of Aircraft", Vol. 24, No. 3,1987, pp. 181-187. https://doi.org/10.2514/3.45414
- Chen A W and Tinoco E N., "PAN AIR Applications to Aero-Propulsion IntegrationR", AIAA-83-1368, 1983.
- Tinoco E N and Chen A W., "Transonic CFD Applications to Engine/Airframe Integration", AIAA-84-0381, 1984.
- CHEN J, WANG H, and ZHANG Y., "Studies on Adaptive Genetic Algorithm Applied to Wing Weight Calculation for Civil Airplanes", Computer Simulation, Vol. 5: 026, 2011.
Cited by
- Development of a Physics-Based Design Framework for Aircraft Design using Parametric Modeling vol.16, pp.3, 2015, https://doi.org/10.5139/IJASS.2015.16.3.370