Platzhalterbild für Chinese Society of Aeronautics and Astronautics

Chinese Society of Aeronautics and Astronautics

Chinese Society of Aeronautics and Astronautics (CSAA) is an academic, non-profit national legal entity based on voluntary membership of scientists and engineers in the field of aeronautics and astronautics. CSAA was established and legally registered in February 1964, providing service related to aeronautics and astronautics for its members. It is a member of the China Association for Science and Technology (CAST) and full member society of the International Council of the Aeronautical Sciences (ICAS) on behalf of the Chinese scientific and technological community.

CSAA now has 350 corporate members and over 130,000 officially registered individual members. There are 56 technical committees, covering nearly all the aeronautical disciplines. Eight member stations were established in member-condensed area to better provide service. Local societies of aeronautics and astronautics were established in 20 provinces, regions and municipalities.

Proceedings of the 8th China Aeronautical Science and Technology Conference Erschienen am 14.02.2026

Proceedings of the 8th China Aeronautical Science and Technology Conference

Volume III · E-Book

Chapter 1: Dynamic Stiffness Analysis for All-Electric Flight Control of EMA Systems.- Chapter2 : Construction of High-Fidelity Real-Scene Three-Dimensional Model for Virtual Proving Ground.- Chapter3 :Methods for Processing and Displaying Finite Element Result Data Based on the HDF5 File Format.- Chapter 4: Effect of Interface Friction and Dimensional Deviation on the Connection Performance of the Thermally Adapted Bolt.- Chapter 5: Research on Surge Boundary Testing and Operation Methods of the 0.6m Continuous Transonic Wind Tunnel Main Compressor.- Chapter 6: Regulation mechanism of shoulder diameter on dynamic recrystallization behavior and mechanical properties of TA2-M pure titanium stir friction lap welded joints.- Chapter 7: Finite Element Analysis of Aircraft Crashworthiness Based on Seat-Occupant-Biomechanical Lumbar Spine Coupling.- Chapter 8: Dynamic modeling and flutter analysis of variable-angle-tow composite for a rectangular wing.- Chapter 9: Simulation of Resin Flow and Process Verification for Complex Multi-Walled Box-Segment Structures in RTM Process.- Chapter 10: Research on Prediction of Monohull Parameters of Surface-Effect Vehicles Based on Machine Learning...

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