Multidisciplinary design optimization of a wide speed range vehicle with waveride airframe and RBCC engine. (15th November 2021)

• Record Type: Journal Article
• Authors: Zhang, Tiantian; Yan, Xiaoting; Huang, Wei; Che, Xueke; Wang, Zhenguo
• Is Part Of: Energy. Volume 235(2021)
• Publication Date: 2021-11-15
• Subjects: MDO -- BLSIO -- Wide speed range -- Optimization -- Aircraft design; Power resources -- Periodicals; Power (Mechanics) -- Periodicals; Energy consumption -- Periodicals; 333.7905
• DOI: 10.1016/j.energy.2021.121386
• Languages: English
• ISSNs: 0360-5442

Abstract

Abstract: The wide speed range vehicle is believed to be ideal for space round trip and its design process incorporates a number of disciplines. To achieve an overall optimal design, we adopt the multidisciplinary design optimization (MDO) approach to design the wide speed range vehicle with waverider being the airframe and the rocket-based combine cycle (RBCC) engine being the propulsion system. The design process includes the modeling of each discipline, the MDO system integration and the operation of the MDO system. Disciplines integrated in the MDO architecture includes the geometry, the aerodynamics, the propulsion, the structural mass and the trajectory. The modeling processes of these disciplines are introduced in brief in this paper and some of them are novel in the relevant area. The Bi-level system integrated optimization (BLSIO) approach is proposed as the MDO strategy, which optimize the trajectory discipline using the state variables of the other disciplines in each iteration process. With an aircraft climb mission being the optimize background, the MDO process is applied successfully and the optimal design obtained by the MDO process reduced the minimum climb time by 10.02% in comparison with the reference model. The analysis shows that the reduce of the minimum climb time is mainly realized by optimizing the configuration of the vehicle and adapting the attack angle in the climb process. The optimal configuration has larger lift-to-drag ratio but fewer fuel remaining after the mission than the reference model. This concludes that although the optimized model is not superior to the reference model in all aspects, it has an overall performance within the design space. Also, the BLSIO approach is ideal in solving the MDO problem of the wide speed range mission. Highlights: A wide speed range vehicle with RBCC engine was optimized by the MDO approach. A thermodynamic model of the RBCC engine was considered for the propulsion subsystem. Bi-level system integrated optimization (BLSIO) approach was proposed as the MDO strategy. The optimized model owns an overall performance within the design space.