APCAT II (Long-Term Advanced Propulsion Concepts and Technologies)[1] is a follow-up of
the previous EC co-funded project LAPCAT [2]. The objective is to develop different vehicle …

Enlarging the range of human displacement is a need in a globalized World where the
commercial, cultural or even recreational links between distinct human settlements are more …

Featured Application This method can be used to quickly predict the overall performance as
well as the meridional flow details of the centrifugal compressors. After being verified, it can …

Mit dem Einsatz mathematischer Optimierungsalgorithmen bei der Auslegung von
mehrstufigen Axialverdichtern können erhebliche Verbesserungen von Wirkungsgrad und …

The air turborocket is a high-speed airbreathing engine that represents an evolution of the
turbojet and rocket motor. The capabilities of the air-turborocket expander were first …

Solidity in compressors is defined as the ratio of the aerodynamic chord over the peripheral
distance between two adjacent blades, the pitch. This parameter is simply the inverse of the …

Throughflow design of multi-stage axial flow compressor still takes the upmost importance
throughout the compressor whole design procedure as it generally fixes 80%∼ 90% of the …

The aerodynamic design of turbomachinery is an exciting engineering problem that involves
a vast design space and requires proficiency in multiple engineering disciplines. For multi …

一维分析模型在离心压气机设计研发中占据重要地位. 基于时间推进求解方法,
发展了离心压气机一维性能分析模型, 并开发了相应计算程序. 为实现性能准确预测 …

In this chapter, optimization of a baseline axial compressor inspired from NASA Rotor 37 is
performed. An in-house optimization code, which utilizes a genetic algorithm is coupled with …