A mechanics model in design of flexible nozzle with multiple movable hinge boundaries
Chengguo Yu,
Zhi Li,
Zhili Zhang,
Licheng Meng,
Guishan Wang,
Yan Shi,
Cunfa Gao
Affiliations
Chengguo Yu
Xi'an Research Institute of High Technology, Xi'an, 710025, China; China Aerodynamics Research and Development Center, Mianyang, 621000, China
Zhi Li
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
Zhili Zhang
Xi'an Research Institute of High Technology, Xi'an, 710025, China
Licheng Meng
China Aerodynamics Research and Development Center, Mianyang, 621000, China
Guishan Wang
China Aerodynamics Research and Development Center, Mianyang, 621000, China
Yan Shi
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China; Corresponding author.
Cunfa Gao
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
In this paper, we propose a modified variational approach to predict the morphology of the flexible nozzle used in wind tunnel. Different from previous studies, the movements of the multiple hinges are considered as movable displacement boundary conditions during establishing the potential energy functional. The cubic spline interpolation method is employed to supply the supplementary boundary conditions in calculation of the functional minimization problem. Current analytical model is verified by experiments carried out on a fixed-flexible nozzle structure whose geometries and materials are the same as those from a commissioned supersonic nozzle. The maximum deviation between the predictions from theoretical method and laser displacement testing does not exceed 0.5 mm. This method can also deal with the large deflection beam problem with multiple movable boundaries.
