Volume 52 Issue 4
Dec.  2022
Turn off MathJax
Article Contents
Suo T, Li Y L, Guo W L. A pioneer of structural strength in aeronautics and astronautics in China — Huang Yushan. Advances in Mechanics, 2022, 52(4): 914-947 doi: 10.6052/1000-0992-22-038
Citation: Suo T, Li Y L, Guo W L. A pioneer of structural strength in aeronautics and astronautics in China — Huang Yushan. Advances in Mechanics, 2022, 52(4): 914-947 doi: 10.6052/1000-0992-22-038

A pioneer of structural strength in aeronautics and astronautics in China — Huang Yushan

doi: 10.6052/1000-0992-22-038
More Information
  • Corresponding author: liyulong@nwpu.edu.cn
  • Received Date: 2022-07-13
  • Accepted Date: 2022-09-06
  • Available Online: 2022-09-07
  • Publish Date: 2022-12-25
  • Professor Huang Yushan was a famous scientist as well as educator in solid mechanics, aeronautics and astronautics in new China. He was enrolled at National Central University in 1931 when he was under 14 years old. He studied for a Ph.D. degree at Stanford University from 1939 to 1940 under the supervision of S. P. Timoshenko, a master in mechanics. As soon as he received his Ph.D. degree, he returned to his motherland without hesitation and was employed as a full professor at National Central University when he was no more than 23 years old. After the founding of New China, even facing to such problems as weak technical foundation, lack of talents and imperfect education system in aeronautics and astronautics engineering, he took infinite pains and devoted his whole life to development of science and technology as well as education. He was regarded as not only the founder of determination, extension of fatigue life and damage tolerance evaluation for in-service aircrafts as well as damage tolerance design for new aircraft, but also the pioneer of self-induced vibration in aeronautics and structural environment strength in astronautics. The article comprehensively overviews the major contributions of Prof. Huang in the area of solid mechanics and structural strength in aeronautics and astronautics, to memorize his firm spirit of serving the nation, rigorous and realistic attitude towards scholarship, courage to be a pioneer, visionary academic perspective, realistic and pragmatic educational thought.

     

  • loading
  • 冯元桢. 1941. 微弯薄曲杆及薄曲板对侧压力之稳定性.[硕士论文]. 南京: 国立中央大学

    Feng Y Z. 1941. Stability of pressure on the opposite side of slightly bent thin curved bar and thin curved plate.[Master Thesis]. Nanjing: National Central University
    郭万林. 1991. 三维断裂和疲劳裂纹扩展.[博士论文]. 西安: 西北工业大学

    Guo W L. 1991. Three dimensional fracture and fatigue crack propagation.[PhD Thesis]. Xi’an: Northwestern Polytechnical University
    黄玉珊. 1941. 弯曲轴与弯曲线. 航空机械月刊, 5: 20-23 (Huang Y S. 1941. The difference between the bending center track and the bending axis. Monthly Journal of Aeronautical Mechanics, 5: 20-23).
    黄玉珊. 1957. 飞机设计中的疲劳问题. 航院学报, 1: 62-66 (Huang Y S. 1957. Fatigue in aircraft design. Journal of Aeronautical College, 1: 62-66).
    黄玉珊. 1958. 多空刚构的柱比分析法. 力学学报, 2: 298-307 (Huang Y S. 1958. Column Analogy for Multi-connected Rigid Frames. Chinese Journal of Theoretical and Applied Mechanics, 2: 298-307).
    黄玉珊, 诸德培. 1963. 边缘受径向集中载荷作用的短悬臂薄壁圆筒壳体. 西北工业大学学报, 1: 53-62 (Huang Y S. 1963. Short cantilever thin-walled cylindrical shell with radial concentrated load on its edge. Journal of Northwestern Polytechnical University, 1: 53-62).
    黄玉珊. 1964a. 整体圆壳筒的Donnell型方程. 西北工业大学学报, 1: 1-6 (Huang Y S. 1964a. Donnell type equation of integral circular shell. Journal of Northwestern Polytechnical University, 1: 1-6).
    黄玉珊. 1964b. 薄圆管在轴压失稳后的极限载荷. 西北工业大学学报, 1: 7-14 (Huang Y S. 1964b. Ultimate load of thin circular tube after axial compression instability. Journal of Northwestern Polytechnical University, 1: 7-14).
    黄玉珊. 1978. 疲劳和断裂的关系. 航空学报, 2: 65-71 (Huang Y S. 1978. Relationship between fatigue and fracture. Acta Aeronauticaet Astronautica Sinica, 2: 65-71). doi: 10.3321/j.issn:1000-6893.1978.02.006
    李玉龙. 1985. 双悬臂梁模型动态裂纹扩展特性的实验研究和分析.[硕士论文]. 西安: 西北工业大学.

    Li Y L. 1985. Experimental investigation and analysis of crack dynamic propagation in double cantilever beam specimens.[Master Thesis]. Xi’an: Northwestern Polytechnical University.
    李玉龙, 刘元镛. 1987. 双悬臂梁模型在阶跃载荷作用下的动态响应及动态断裂韧性KId(σ)的确定方法. 西北工业大学学报, 4: 469-479 (Li Y L, Liu Y Y. 1987. The determination of dynamic response and dynamic fracture toughness KId(σ) of DCB model under step loading. Journal of Northwestern Polytechnical University, 4: 469-479).
    林富甲, 黄玉珊. 1982. 裂纹检测概率曲线的统计测定. 航空学报, 4: 21-27 (Lin F J, Huang Y S. 1982. Statistical determination of a flaw detection probability curve. Acta Aeronauticaet Astronautica Sinica, 4: 21-27). doi: 10.3321/j.issn:1000-6893.1982.04.003
    林富甲, 黄玉珊. 1983. 成对使用的机翼主要构件可靠性分析. 航空学报, 4: 19-27 (Lin F J, Huang Y S. 1983. Reliability analysis for paired main wing components. Acta Aeronauticaet Astronautica Sinica, 4: 19-27). doi: 10.3321/j.issn:1000-6893.1983.03.003
    刘雪惠, 黄玉珊. 1983. 半线性Willenborg迟滞模型. 西北工业大学学报, 1: 71-78 (Liu X H, Huang Y S. 1983. Semi-Linear Willenborg Retardation Model. Journal of Northwestern Polytechnical University, 1: 71-78).
    Broek D, Smith SH. 1979. The prediction of fatigue-crack growth under flight-by-flight loading. Eng. Fract. Mech., 11: 123-141.
    Elber W. 1971. The significance of fatigue crack closure. ASTM STP486, 230-242.
    Fung YC, Kaplan A. 1952. Buckling of low arches and curved beams of small curvature. NACA TN2840.
    Huang YS. 1939. Stiffeners of beams and cables. Aircraft Eng., 8: 314.
    Huang YS. 1940. Bending of rectangular plates having forces in the middle planes of the plates.[PhD Thesis]. Palo Alto: Stanford University.
    Huang YS. 1941. Buckling of plates with lateral stiffeners. J. Royal Aero. Society, 45 (370): 326-330.
    Lévy MM. 1899. Sur l’équilibre élastique d’une plaque rectangulaire. Comptes Rendus, 15: 535-540.
    Li YL, Liu YY, Huang YS. 1985. The calculation of stress intensity factor of DCB model using distorted isoparametric elements. Conference Proceedings of the Mechanism of Fracture, ASM: 135-138.
    Paris P, Erdogan F. 1963. A critical analysis of crack propagation laws. J. Basic Eng. Trans. Am. Soc. Mech. Eng., 528-534.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(14)

    Article Metrics

    Article views (1953) PDF downloads(155) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return