Zong Pu's writing background, personal information and his brother's information about Wisteria Falls.

Brief introduction of China science and technology experts

Zong Pu (Pú) (1928-), female, formerly known as Feng Zhongpu, pen names Ren Xiaozhe and Feng Fei. The daughter of the famous philosopher Feng Youlan, 1928 was born in Beijing in July, and moved to Kunming with her family when she was ten years old. I went to Nanjing Primary School and The National SouthWest Associated University High School. 1946 was admitted to the Foreign Languages Department of Tianjin Nankai University, and then transferred to the Foreign Languages Department of Tsinghua University. 195 1 graduated. Worked in China Federation of Literary and Art Circles, Literature and Art Newspaper and other units. 1960 tune world literature editorial department. Before the Cultural Revolution, his works mainly included short stories Red Bean, Peach Blossom Garden, Daughter Marries My Valley, Mirror Lake, Back Door and Companion. Red beans were criticized inappropriately. After the Cultural Revolution, there were the short story A Dream on a String and the novella Sanshengshi, which won the national excellent novella award. 198 1 Selected Novels and Proses of Zong Pu published by Beijing Publishing House. Later, he struggled to create a novel "Wild Hulu Yin" reflecting the fate of China intellectuals, and the first novel "Dunan Ji" was published on 1987, which was well received. 1948 began to publish his works, and became famous in 1957 with the short story Red Bean. In the new period, a large number of works have been published, including the short story Dream on a String (won the National Excellent Short Story Award 1978), the novella Sanshengshi (won the First National Excellent Novelette Award), the fairy tale Zongpinfish (won the First National Excellent Children's Literature Award by the Chinese Writers Association), Dwelling House, Who am I, etc. 1988, the first novel "Du Nanji" was published, 1996, the four-volume "Collected Works of Zong Pu" was published by Huayi Publishing House. In recent years, he has created a series of novels "Introduction to Wild Gourd" reflecting the fate of intellectuals in China. Zong Pu has absorbed the essence of China traditional culture and western culture, and has profound knowledge and unique charm. Her novels are deliberately innovative, with bright and implicit language, smooth and lingering, and quite distinctive. Her prose is as profound and meaningful as water. Zong Pu worked hard in his illness for seven years, and the second part of Dunan Collection, Dong, finally came out. There are also The Journey to the West and Journey to the North in the plan, which are multi-volume series with the total title of Biography of Wild Gourd. Zong Pu established a beautiful and gentle language style with his meticulous and calm narration. The fate of many characters and the mentality of the world are slowly unfolding in seemingly dull life situations and details, and the layout is magnificent. Zong Pu's war has no swords and swords, but it has been branded with deep mental scars and has a vivid scroll atmosphere. The cultural texture immersed in bone marrow actually makes people feel that they are in the context of A Dream of Red Mansions. Reading such a meaningful and exquisite novel by Dong is really a kind of enjoyment.

Zong Pu's article "Wisteria Falls". Zong Pu's family was persecuted during the Cultural Revolution, and "anxiety and grief" haunted the author all the time. This article was written in May, 1982. At that time, the author's little brother was terminally ill. The author is very sad (his little brother died in June, 1982). He wandered in the yard and saw a wisteria in full bloom. He let nature take its course, flowers turned from decline to prosperity, from sadness to joy, and realized the beauty and eternity of life, so he wrote this article.

Zong Pu's brother's message.

Feng Zhongyue, an expert on aircraft structural strength, said. Long-term engaged in aircraft structural design and strength research. He has made important contributions to the structural strength calculation and test of new fighters, the development of aviation structural analysis system (HAJIF) and the modernization of static, dynamic and thermal strength tests of aviation structures.

Feng Zhongyue was born in Beiping (now Beijing). Originally from tanghe county, Henan. Grandfather Feng Taiyi was a scholar in Qing Dynasty and served as a magistrate in Chongyang, Hubei Province. His father, Feng Youlan, is a deputy to the Fourth National People's Congress, a member of the Second, Third and Fourth CPPCC, and a member of the Standing Committee of the Sixth CPPCC, Professor Peking University. He is a famous scholar at home and abroad. Ren Zaikun, a mother, graduated from Beijing Women's Normal School and is the daughter of Ren Zhiming, a pioneer of the Revolution of 1911. Feng Zhongyue completed all his studies in Kunming and Beijing, from primary school to middle school to university. 1952 graduated from Tsinghua University aviation department. In college, he was an active member of China * * * Production Party, and 1952 joined China * * * Production Party.

When Feng Zhongyue began to work and live, it was just that People's Republic of China (PRC) had just been established, the prelude of national economic construction had just begun, the first five-year plan began to start, and the aviation industry as a new industrial sector began to build. As a * * * party member, he gave up his desire to stay in Kunming to study and work, resolutely signed up to obey the organizational distribution and went to the place where the country needed it most, so he was assigned to Shenyang Aircraft Factory and joined the ranks of building aviation industry.

At that time, according to the development policy determined by the central government, from repair to manufacturing and from imitation to self-design, after completing the transformation from repair to manufacturing, the aviation industry began to build aviation scientific research institutions and carry out research and design work from 1955. 1956, the first aircraft design room was established, and Feng Zhongyue began to study the structural strength of aircraft.

During the 25 years of studying the strength of aircraft structure in Feng Zhongyue, with the continuous progress of science and technology and the improvement of aircraft tactical and technical performance, the layout of aircraft structure has changed constantly, and some traditional theoretical methods are no longer applicable in strength calculation. Therefore, opening up new fields, researching new technologies and achieving new breakthroughs to meet the needs of developing new aircraft have become the main topics of aircraft structural strength research. In addition, with the increasing use of electronic computers, the research of application software has become an important topic of strength research. In this situation, Feng Zhongyue made progress despite difficulties, made progress on the road of scientific research with tenacious fighting spirit, achieved one achievement after another, overcame one technical difficulty after another, promoted the continuous progress of aircraft structural strength research, and made contributions to the development of aviation scientific research in the motherland.

An important feature of Feng Zhongyue's scientific research work is that he can grasp the scientific and technological development trend of his major, determine the main direction of scientific research, and plan the research topic of aluminum. Once the research topic is determined, he will personally organize the implementation and take the lead in tackling key problems. He has both strategic thoughts and tactical goals; He is both a commander and a combatant. In scientific research management, he has the overall situation, decisive command and step by step. He is strict with scientific and technical personnel, meticulous, set an example and arrive as scheduled. When reviewing the report, he has to check the mathematical formulas one by one, even punctuation and typos.

An important contribution of Feng Zhongyue in scientific and technological work is to train a group of people and a group of scientific and technological workers. We should not only boldly let go, but also guide scientific and technological personnel to bear the burden and embark on the subject in time, so that they can grow their talents in the practice of scientific and technological work. He is very concerned about the updating of scientific and technological personnel's knowledge and the improvement of foreign language level, and gives them opportunities for further study. He pays special attention to the discovery and training of top technicians. Liu, a middle-aged science and technology expert with outstanding contributions at the national level, was one of the top technical talents trained at that time.

Feng Zhongyue himself wrote: "I think I have a strong spirit of seeking knowledge and am sensitive to new things, so I can make some directional suggestions to support those creative ideas. Because I have been exposed to many technical fields and have a wide range of knowledge in these years, I can solve some technical difficulties and organize and guide the research and implementation of large-scale technical projects. " Because of his achievements in scientific and technological work, he grew up to be the first generation of aircraft structural strength experts in the motherland. He was elected as a director of China theoretical and applied mechanics Society, a director of China Aviation Society and a member of the Science and Technology Committee of the Ministry of Aviation Industry. 198 1 was promoted to senior engineer.

Feng Zhongyue's achievements in science and technology make him a veritable expert. He has outstanding literary accomplishment, likes literature and art, and is good at poetry, calligraphy and seal cutting. When he died, Feng Youlan wrote an elegy for his son:

"Is a good party member, a good cadre, ambitious,

Tears only hurt for home;

Being proficient in science and technology, being proficient in literature and art, all talents are rare.

Evocation is hard to come back. "

Feng Zhongyue struggled for China's aviation scientific research all his life, leaving valuable material wealth and spiritual wealth for future generations.

Pioneer of aircraft structural strength work

After the founding of People's Republic of China (PRC), 195 1 started to build the aviation industry, and 1956, China has already manufactured jet planes. On this basis, it has been put on the agenda of aviation industry to develop aviation scientific research, independently design and manufacture its own aviation products and realize the transformation from imitation to independent design.

1956, the aircraft design room of Shenyang Aircraft Factory was established, and the design of China's first jet trainer -J 1 aircraft was started. Feng Zhongyue is the strength director of the aircraft design room, responsible for the strength work of 1 aircraft. Presided over the formulation of strength calculation scheme, issued the main design drawings, drafted and issued the outline and task book of static test of the whole machine, and assisted the laboratory leaders in organizing the preparation of static test of the whole machine. The static test of J- 1 aircraft passed smoothly, and the strength was completely qualified, which laid a solid foundation for the flight test of the new aircraft.

1958 In the summer, entrusted by the leaders, Feng Zhongyue braved the hot summer to come to Nanchang Aircraft Factory to participate in the strength evaluation of Chujiao 6 aircraft designed and manufactured by China. The static test of the whole aircraft proves that the aircraft after review and strengthening meets the strength requirements.

After 1958, Feng Zhongyue participated in the design of two high-altitude high-speed fighters. Both of these aircraft are wings with low aspect ratio, and the traditional engineering beam theory can no longer be used for stress analysis of this type of wing. He used the matrix displacement method with the beam and torsion box as the basic units, and used the computer to analyze the stress of Dongfeng 1 13 aircraft. At the same time, the application of matrix force method is also discussed.

1961August After the establishment of the Aviation Research Institute, Feng Zhongyue was appointed as the deputy director of the Power Room of the Fighter Design Institute (the director in 1962). At that time, the main task was to understand (digest) the MIG -2 1 aircraft imported from the Soviet Union and create conditions for designing new fighters in the future. He organized and led the translation and digestion of MiG -2 1 aircraft strength calculation report, so as to master the characteristics of this type of aircraft strength calculation. In order to verify its calculation method, the experimental research work of some specimens was organized and guided. In the process of understanding MIG -2 1 aircraft, he was not satisfied with knowing only the general situation of the aircraft, but asked to know the calculation parameters, load types, calculation methods, calculation results, material selection and handling of aerodynamic heating problems selected in the Chu Yuan Report. This is undoubtedly necessary for engineers and technicians who have no experience in supersonic aircraft design. In the process of understanding, the inconsistency of data in the original report and the error of calculation data were corrected, and the consistency of data and drawings was ensured, so that the aircraft factory had a complete and correct strength report as a basis for dealing with production problems.

In order to meet the needs of developing a new aircraft by himself, he absorbed the strength calculation report of MIG -2 1 aircraft, attached importance to introducing new technologies, personally participated in and organized scientific and technical personnel to study the stress analysis and influence coefficient of the wing with low aspect ratio, and compiled a program for the analysis and calculation of the stress and deformation of the wing based on the direct stiffness method. In addition, he also led the application research and optimization design of honeycomb structure, integral panel and new materials, which made technical reserves for designing new fighters.

1964, China began to design the first high-altitude high-speed fighter-J-8 aircraft. In the design of J-8 aircraft, Feng Zhongyue is responsible for the structural strength and testing of the whole aircraft. According to the actual situation of aircraft design in China, he formulated the "Strength Calculation Principle of J-8 Aircraft" and determined the calculation scheme of the main components of the aircraft. He stressed that it is necessary to "bring forth the old and bring forth the new" on the basis of absorbing the successful calculation methods of MIG -2 1 aircraft, and make full use of the scientific research achievements already made to achieve a new breakthrough in the strength calculation level of the J-8 aircraft. MiG-2 1 aircraft is used for wing design and calculation, the influence coefficient is given by LCVY displacement method, and the finite element method is used for checking calculation. The strength calculation of the fuselage still adopts the traditional simplified assumption. Feng Zhongyue released the main design drawings of the J-8 aircraft. In order to ensure the design quality and the safety of the aircraft, he organized a series of experimental research work. The static test of the whole aircraft proves that the strength work of the J-8 aircraft is successful. Feng Zhongyue's strength calculation principle and practice for J-8 aircraft were later used for reference or used in the development of other new aircraft.

The J-8 aircraft won the 1985 National Science and Technology Progress Special Prize. As Feng Zhongyue is the main participant in the development of the J-8 aircraft, he has made important contributions to the design of the J-8 aircraft. 1in June, 1987, the National Science and Technology Progress Award Evaluation Committee awarded him a special award.

After 1970, Feng Zhongyue participated in the demonstration of the design scheme of the J-9 aircraft. Because the flight speed of the J-9 aircraft has exceeded the thermal barrier, he turned the focus of his research work to the thermal structure, especially the specification and strength calculation standard of the thermal structure.

1973, organized and led the static fault tests of Shuihong 5, Yun 7, Yun 8 and Yun 10. All these experimental projects have been successful and met the requirements of design and production units.

China is a pioneer in the application research of finite element method.

The research and application of finite element method is put forward from the actual needs of aircraft design. 1958, China began to design two supersonic fighters-Dongfeng 107 and Dongfeng 1 13. Because these two kinds of aircraft are wings with low aspect ratio, the traditional engineering beam theory can not be used to calculate the strength and stiffness of these aircraft wings. At that time, the problem faced by Feng Zhongyue was that it was necessary to find the calculation method of the wing with low aspect ratio to solve this key technical problem in aircraft design.

As we all know, there are two major problems in the strength and stiffness of low aspect ratio wings: first, the relative thickness is small and the stress level is high, which requires higher accuracy of stress analysis. However, due to its complex structure and small internal space, it is necessary to hang various control surfaces (flaps and ailerons) in addition to providing landing gear and storing fuel tank, so the engineering calculation method based on plane assumption is no longer applicable and a new structural analysis method must be sought. Secondly, the flutter analysis of the wing with low aspect ratio is a key to the design, and the flutter analysis was based on the accurate matrix of the influence coefficient of structural flexibility (traditional engineering calculation methods can not do it). That is to say, we must find a method that can not only give accurate stress and deformation, but also give the flexibility influence coefficient matrix of the structure.

In order to solve this key technical problem, Feng Zhongyue read a lot of literature and found that the international community has just begun to explore ways to solve this problem. Among different opinions, Feng Zhongyue thinks that the matrix method of structural analysis is the way out. So he organized manpower to carry out research work, studied and discussed with everyone, made clear the principle of the method and tried examples. At that time, there was only one handheld computer in the design room, and it often took a week to calculate a matrix algebraic equation of order 10. Through a period of exploration, the matrix method of structural analysis has been initially introduced, and the basic principles and calculation steps of displacement method and force method have been mastered.

196 1 Establishment of Aviation Research Institute (the Sixth Hospital of the Ministry of National Defense). Feng Zhongyue submitted his own report on "Study on Strength and Stiffness of Wings with Small Aspect Ratio" to the Sixth Academy in time. The Sixth Hospital approved Feng Zhongyue's report, which was included in the scientific research plan as the key research topic of the Sixth Hospital. He personally served as the project leader, guiding the research work of the project ideologically and technically. The members of the research group are stationed in Beijing to tackle key problems, and they have received strong support from the Institute of Computing Technology of Chinese Academy of Sciences.

In the research of this subject, Feng Zhongyue's attitude towards scholarship is rigorous, and he not only attaches importance to theoretical research, but also attaches importance to experimental verification. At the same time, he overcame all difficulties and personally organized forces to make a metal model of 1: 5 for comparative analysis. Then it is difficult to measure the influence coefficient of wing structure, which lays the foundation for the smooth development and subsequent success of the research work.

After three years' efforts, the project "Study on Strength and Stiffness of Wings with Low Aspect Ratio" successfully completed the research tasks specified in 1965, and submitted corresponding finite element analysis programs which can be used for model design, such as displacement method, force method, direct stiffness method and substructure analysis method, which were basically close to the international level at that time.

Starting from 1964, China developed its own J-8 aircraft. Feng Zhongyue decided to use the self-developed finite element method to check and calculate the J-8 wing, which made our country's aircraft design adopt its own characteristic, advanced and reliable analysis method, and made the electronic computer get practical application in our country's designed aircraft. This research achievement won the National Science Conference Award of 1978.

Structural Analysis System —— A Milestone of Computational Mechanics in China

1in April, 1975, the Sixth Hospital of No.3 Machinery Department held a ten-year planning meeting on aircraft and tactical missile force research in Xi 'an. According to the development trend at home and abroad and the urgent requirements of all aspects, Feng Zhongyue thinks that China has the conditions to develop a large-scale general structural analysis system, and suggests that the development of a general finite element aviation structural analysis system should be the key subject of strength research. The Institute agreed and approved Feng Zhongyue's suggestion, and included the research topic of aviation structural analysis system in the research work plan of the Institute, and appointed Feng Zhongyue as the first, second and third chief engineers of structural analysis system.

Type I aviation structural analysis system (HAJIF 1 for short) is a software system for structural static analysis. Development began in May 1976, and passed the ministerial appraisal in September 1979. It is the first large-scale, universal and efficient aerostatics structural analysis application software system successfully developed in China.

Type I structural analysis system can analyze the deformation and stress of the structure under aerodynamic load, concentrated load and inertial load. The system adopts original multi-layer substructure and local symmetry analysis technology, which is universal and easy to analyze large and complex structures with arbitrary shapes. The system has established a user-oriented special language for structural analysis, which is flexible to use, easy to master and convenient to organize special programs. The system has the ability to automatically generate data, which greatly reduces manual labor. The system provides two solutions: automatically adding valid columns and metamatrices in blocks. The system adopts modular structure, which is convenient for system expansion and modification. The system has the functions of interruption and diagnosis.

After the structural analysis system I was put into use, it improved the analysis ability of large aviation structures and provided a powerful scientific calculation method for aircraft strength design and research, thus improving the design quality of aircraft and shortening the development cycle. It is an indispensable basic work to realize the modernization of aviation technology. The appraisal thinks: "It is the first time in China to solve large-scale complex structures by computer and establish an automatic program system for structural analysis, which fills the gap in China and is a major scientific research achievement in the aviation industry, which is of great significance to the development of new aircraft." Qian Lingxi of Dalian University of Technology pointed out: "The successful development of structural analysis system I is a milestone in computational mechanics in China." This achievement won the first prize of 1979 Third Machinery Department and the National Defense Industry Office, and the second prize of 1985 National Science and Technology Progress Award.

Structural Analysis System II (Hajif-II) is a software system for dynamic analysis of aviation structures. The system was developed in 1979, 1 1 and passed the ministerial appraisal in 198 1.

The dynamic analysis system of aviation structure has the functions of calculating the natural vibration characteristics of the structure, flutter calculation of active control system and local gust response calculation. Its scale includes 28,000 FORTRAN statements, 27 modules and 3 1 fixed processes. The structural model can have 7000 degrees of freedom, and 70 feature vectors can be calculated. In unsteady aerodynamic calculation, the number of aerodynamic blocks per airfoil can reach 200, and five airfoils can be calculated. There are as many as 50 tables used in flutter and gust response calculation.

The system is the first dynamic analysis system of aviation structure in China, which has been proved to be reliable by practical use and can meet the urgent needs of natural vibration and aeroelasticity analysis of aviation structure at present. In mechanics, numerical calculation and program design, many new technologies at home and abroad in the late 1970s have been adopted, which have advanced domestic level. This achievement won the second prize of 198 1 No.3 Machinery Department's scientific and technological achievements and the second prize of 1985 National Science and Technology Progress Award.

Structural Analysis System III (Hajif-III) is a software system for nonlinear analysis of aviation structures. 1977 demonstration, 198 1 year development, 1985 passed the ministerial appraisal. Feng Zhongyue died of illness in June 1982 after completing the demonstration, setting up a research group and starting research work.

Type Ⅲ structural analysis system has nearly 80,000 FORTRAN statements, and has relatively complete nonlinear analysis function. It has some originality in automatically selecting the load increment step size and automatically determining the degree of freedom of nodes. This system fills the gap in the nonlinear analysis system of large-scale structures in China and reaches the advanced level abroad in the early 1980s. This achievement won the first prize of 1987 National Science and Technology Progress Award.

While developing HAJIF system, Feng Zhongyue also organized and directed the development of structural multi-constraint optimization design system. This work started at 1979 and ended at 198 1. The successful development of the system organically combines advanced finite element analysis with mathematical programming methods, which provides an effective means for aircraft structure verification and design. The project won the first prize of 1988 ministerial achievements and the second prize of 1985 national scientific and technological progress.

Committed to the modernization of aviation technology

After the Third Plenary Session of the Eleventh Central Committee of the Communist Party of China, the modernization of industry, agriculture, national defense and science and technology has been put on the agenda of socialist construction. A journey of a thousand miles begins with a single step. At this time, what Feng Zhongyue is thinking about is how to change the backward appearance of aircraft strength work, realize the modernization of test and calculation means as soon as possible, and even the modernization of the whole aircraft design and manufacture. He thinks that the technical equipment in our laboratory is outdated, and if we want to carry out experimental research, we must update the equipment.

From 65438 to 0979, Feng Zhongyue visited the scientific research institutions and aircraft companies in the United States and the Federal Republic of Germany twice, and learned about the current situation and development level of aircraft strength research in the two countries. He read other people's books, but he thought more about how to develop himself. He said: "The most important measure and standard is the breadth and depth of computer application." In his view, we should not wait for hardware in strength research, but catch up with the development of software as soon as possible and promote the development of hardware. It is necessary to speed up the computerization of experimental technology. We should concentrate manpower and financial resources to gradually realize the computerization of experimental technology and change the backward state of manual operation at present.

Aircraft structural strength research institute is responsible for the qualification test and fatigue, vibration and transient thermal stress test of large aircraft, but the existing test equipment is backward in technology, low in efficiency, large in error and long in test period, which is difficult to meet the requirements of test work. He actively suggested to the leaders of the Ministry and Academy that the necessary advanced equipment should be introduced from abroad to speed up the modernization process of strength research. With the approval of the Ministry leaders, Feng Zhongyue formed a special working group to investigate and demonstrate the imported projects, so that the imported projects are advanced in technology and reasonable in price.

In order to solve the backward state of transient thermal stress test equipment, 1977 12 signed a contract with Hitachi, Japan, and introduced Hitachi -80 computer system, that is, computer-controlled heating loading and real-time data acquisition and processing system for transient thermal stress test. After the equipment is put into use, the transient thermal stress testing technology is in the leading position in China.

With the rapid development of aviation science and technology, higher requirements are put forward for fatigue test technology. Compared with the analog hydraulic servo loading system controlled by foreign digital computers, there is a big gap in performance, safety and reliability between analog and digital-analog automatic coordinated loading equipment developed in China. In order to change this backward situation, the Ministry approved the introduction of 100 channel CNC coordinated loading system from MTS company in the United States. The system can be used for fatigue test of 120 ton large aircraft and is compatible with static test. This is a relatively advanced fatigue test equipment in China at that time.

In order to realize the modernization of aircraft design and manufacturing, after a major breakthrough in the development of aviation structure analysis system, Feng Zhongyue turned its research direction to the field of realizing aircraft design and manufacturing automation, that is, developing computer-aided design and manufacturing system. In order to find the basis and learn from foreign experience, he took this topic as one of the focuses of his visit to the United States during 1979. On the basis of collecting a lot of information at home and abroad, this paper makes a systematic demonstration, and personally writes the demonstration report "The Development Path of Computer Aided Design and Aided Manufacturing". 1980, Feng Zhongyue formally proposed to the leaders of the Ministry and Academy that "based on the existing domestic hardware, seize the opportunity to carry out computer-aided design and manufacturing", which was quickly supported and endorsed by the leaders of the Ministry and Academy. At the end of 1980, the 7760CAD/CAM research group was established, and the Ministry appointed Feng Zhongyue as the chief engineer of the research group. 198 1 year, he braved the summer heat to travel to Beijing, Shenyang, Xi, Chengdu and other places to carry out investigations and joint research. At the beginning of the development of 7760CAD/CAM, 1982+00 June, Feng Zhongyue passed away. 7760CAD/CAM system 1986 was successfully developed, and 1988 won the second prize of National Science and Technology Progress Award.

(Author: Zhang)

Biographical notes

L93 1 year 65438+February 3 1 was born in Beiping (now Beijing).

1952 graduated from Tsinghua University aviation department. He used to be the director of the process room of the assembly workshop of Shenyang Aircraft Factory, and later served as the strength leader of the design department of the factory.

65438-0956 served as the strength leader of the aircraft design room of Shenyang Aircraft Factory.

196 1 served as deputy director of the strength room of fighter design institute of aviation research institute of national defense, 1962 as director, 1965 as director in charge of structure, strength and test work.

From 65438 to 0970, he served as the director of the strength room of Chengdu Fighter Design Institute in Sichuan.

1973 deputy director and chief engineer of aircraft structural strength research institute.

1982 10 died in Beijing.

Main thesis

1 Feng Zhongyue. Influence coefficient and structural analysis of delta wing. Aviation technical reference, 1960.

Feng Zhongyue. Aeroelasticity of wings with low aspect ratio international aviation, 1960.

Feng Zhongyue. Introduction to aeroelasticity. Beijing: National Defense Industry Press, 1963.

4 Feng Zhongyue. Parametric method of fighter fatigue analysis, foreign aviation technology, 1973.

5 Feng Zhongyue. Elastic-plastic analysis method. Finite element method in solid mechanics (translation set), Beijing: Science Press, 1977.

Feng Zhongyue. Application of computational images in product structure analysis. Finite element method in solid mechanics (translation set), Beijing: Science Press, 1977.

Feng Zhongyue. Application of computer-controlled servo hydraulic test equipment in large-scale structure verification test. Foreign aviation technology, 1979.

Feng Zhongyue. Type I aviation structure analysis system for static analysis. Journal of Aviation, 1980 (1).

Feng Zhongyue. A computer program to simulate the structural crash of an airplane. International aviation, 198 1 (9).

Feng Zhongyue 10. Application of finite element method in China aviation structure analysis. British finite element news,1981(2,3).