Thermal Management and Fuel System Model for TBCC Dynamic Simulation
Thermal Management and Fuel System Model for TBCC Dynamic Simulation
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DOI：
10.2514/6.2010-6642
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发表时间：
2010-07
期刊：
影响因子：
2.5
通讯作者：
E. Gamble;Daniel A. Haid
中科院分区：
文献类型：
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作者：
E. Gamble;Daniel A. Haid
* * SPIRITECH Advanced Products，Inc，Tequesta，佛罗里达正在开发一种动态模拟器，用于演示涡轮基联合循环（TBCC）推进系统的所有超音速运行模式，包括模式转换。高马赫瞬态发动机循环代码（HiTECC）是一个高度集成的仿真工具，它由每个TBCC系统的模型组成，TBCC系统的性能和可控性影响推进系统的推力和可操作性。报告的工作详细介绍了在多年努力开发动态TBCC模拟器的第二年进行的热管理和燃料系统模型的开发。一旦完成，这个模型将大大扩展所有TBCC工作模式的最新技术水平，通过提供系统的数值模拟，相互作用和瞬态响应影响推进系统的能力，从涡轮发动机为基础的冲压/超燃冲压发动机为基础的推进过渡。
*† SPIRITECH Advanced Products, Inc, Tequesta, Florida A dynamic simulator is being developed to demonstrate all modes of supersonic operation, including mode transition, for a Turbine-Based Combined Cycle (TBCC) propulsion system. The High Mach Transient Engine Cycle Code (HiTECC) is a highly integrated simulation tool comprised of models for each of the TBCC systems whose performance and controllability affect the thrust and operability of the propulsion system. The reported work details the development of the Thermal Management and Fuel System model conducted in the second year of a multiyear effort to develop a dynamic TBCC simulator. Once completed, this model will significantly extend the state-of-the-art for all TBCC modes of operation by providing a numerical simulation of the systems, interactions, and transient responses affecting the ability of the propulsion system to transition from turbine-based to ramjet/scramjet-based propulsion.