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Tag: General – Turbomachinery

Stage Number Selection in Axial Aircraft Turbines

Choosing the number of stages during the development of axial turbines is one of the most controversial design tasks because it has many options...

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Gas Turbine Cooling System Design Procedures

IntroductionState-of-the-art gas turbine engines usually work under extremely high temperatures. This is directly related to efficiency of the gas turbines – in order to...

Turbomachinery Evolution through Generative Design

As human-beings, our differences are what makes us unique (if I may quote the Seek Discomfort crew – “What makes you different is what...

Challenges in Aero Engine Performance Modeling

As is the case with every machinery, manufacturers want to improve their products. This is especially true for aero engines, where even a small...

The Evolution of Gas Turbines From the First Designs to the Latest Environmentally Friendly Development Trends: Part 2

Part 1Gas Turbine Development Trends: Hydrogen EnergyRecent world trends related to the development of clean energy have led to an increased focus on...

The Evolution of Gas Turbines From the First Designs to the Latest Environmentally Friendly Development Trends: Part 1

Part 2Gas turbines have a rich history and play a key role in many of the modern-day technology we rely on. Welcome to...

How Work Distribution Between the Stages of an Axial Multistage Compressor Affect Compressor Characteristics

One of the important factors affecting compressor performance is the distribution of work between compressor stages.There can be many different axial compressors with the...

Rocket Nozzle Cooling

It is impossible to imagine the design of any rocket engine without a nozzle – a technical device that serves to accelerate gas flow...

Inducer Design Considerations and its Effect on Turbopump Cavitation

Why Use an Inducer? Suppose you want to build a turbopump to increase the pressure of your working fluid. However, you find that the fluid that you are working with keeps vaporizing in the impellers you design, causing all sorts of performance issues. What can you do in this case? One solution is to design Read More...

The post Inducer Design Considerations and its Effect on Turbopump Cavitation first appeared on Turbomachinery blog.

Drilled Nozzle Application in Supersonic Turbines

Most designers associate drilled nozzles in turbomachinery with something exotic, uncharted, and specific only to a minuscule amount of high-loaded turbines operating with a high-pressure drop. Meanwhile, many engineers are not aware that this nozzle design has been applied since the very first turbomachines. Karl Gustaf Patrik de Laval patented a turbine with asymmetric convergent-divergent Read More...

The post Drilled Nozzle Application in Supersonic Turbines first appeared on Turbomachinery blog.

Turbo-compressor Technologies for Aviation Fuel Cell Systems: Operational Requirements and Development Trends

Introduction Fuel cells are an important driver in the current energy system landscape with significant impact on the technology base and economic growth. Global fuel cell system shipments saw a 10% increase in 2020, totaling 1.3GW. The transport sector continues to lead with a growth of 25% on the number of units shipped globally. The Read More...

The post Turbo-compressor Technologies for Aviation Fuel Cell Systems: Operational Requirements and Development Trends first appeared on Turbomachinery blog.

An Introduction to Shock Waves

When you think of shock waves, I would wager that you picture a supersonic jet zooming past overhead. Or maybe you have experienced the famous (or infamous) “sonic boom” that accompanies shock waves attached to airplane engines. The engineering challenges associated with the often-troublesome behavior of shock waves is present in all scales, from carefully Read More...

The post An Introduction to Shock Waves first appeared on Turbomachinery blog.

Scaling and Trimming in Axial Compressors and Fans

Introduction Despite the deepening understanding of the essence of gas-dynamic processes and the development of computational methods, simpler design methods such as scaling and trimming remain in demand in turbomachinery engineering. The main advantage of these approaches over design from scratch is simplicity and its inexpensive nature due to the small-time expenditure and lower demand Read More...

The post Scaling and Trimming in Axial Compressors and Fans first appeared on Turbomachinery blog.

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