Modelling of Liquid-Fuelled Rotating Detonation Engines for Gas-Turbine Applications Scholarship – Eligibility, Benefits & How to Apply

🌟 About the Scholarship

Opens
Closes30 Jun, 2026

The Modelling of Liquid-Fuelled Rotating Detonation Engines for Gas-Turbine Applications Scholarship is a fully funded PhD research opportunity offered by the University of Southampton in the United Kingdom. The scholarship operates under the EPSRC Industrial Doctoral Landscape Award (IDLA) framework, supported by EPSRC. It provides full funding for doctoral research, including tuition support and financial maintenance. In addition, students gain access to a strong industrial research environment and advanced computational resources at the University of Southampton. Furthermore, the program includes training in combustion modelling, numerical methods, high-performance computing, and aerospace propulsion systems.

🎓 Scholarship Snapshot

Here’s everything you need at a glance: the documents to prepare, what the award covers, and key dates so you don’t miss a beat. From transcripts and essays to tuition and living support, this gives you a clear picture of the Modelling of Liquid-Fuelled Rotating Detonation Engines for Gas-Turbine Applications Scholarship before you apply.

Eligible Countries

Afghanistan, Albania, Algeria, Andorra, Angola, Antigua and Barbuda, Argentina, Armenia, Aruba, Australia, Austria, Azerbaijan, Bahamas, Bahrain, Bangladesh, Barbados, Belarus, Belgium, Benin, Bhutan, Bolivia, Bosnia-Herzegovina, Botswana, Brazil, Brunei Darussalam, Bulgaria, Burkina Faso, Burundi, Cabo Verde, Cambodia, Cameroon, Canada, Cape Verde, Central African Republic, Chad, Chile, China, Colombia, Comoros, Costa Rica, Côte d’Ivoire, Croatia, Cuba, Cyprus, Czech Republic, Democratic Republic of the Congo, Denmark, Djibouti, Dominica, Dominican Republic, East Timor, Ecuador, Egypt, El Salvador, Equatorial Guinea, Eritrea, Estonia, Eswatini, Ethiopia, Fiji, Finland, France, Gabon, Gambia, Georgia, Germany, Ghana, Greece, Greenland, Grenada, Guam, Guatemala, Guinea, Guinea Bissau, Guyana, Haiti, Honduras, Hong Kong, Hungary, Iceland, India, Indonesia, Iran, Iraq, Ireland, Israel, Italy, Jamaica, Japan, Jordan, Kazakhstan, Kenya, Kiribati, Kosovo, Kuwait, Kyrgyzstan, Lao People’s Democratic Republic, Laos, Latvia, Lebanon, Lesotho, Liberia, Libya, Liechtenstein, Lithuania, Luxembourg, Madagascar, Malawi, Malaysia, Maldives, Mali, Malta, Marshall Islands, Mauritania, Mauritius, Mexico, Micronesia, Moldova, Monaco, Mongolia, Montenegro, Morocco, Mozambique, Myanmar, Namibia, Nauru, Nepal, Netherlands, New Zealand, Nicaragua, Niger, Nigeria, Niue, North Korea, North Macedonia, Norway, Oman, Pakistan, Palau, Palestine, Panama, Papua New Guinea, Paraguay, Peru, Philippines, Poland, Portugal, Puerto Rico, Qatar, Romania, Russia, Rwanda, Saint Kitts and Nevis, Saint Lucia, Saint Vincent and the Grenadines, Samoa, San Marino, Sao Tome and Principe, Saudi Arabia, Scotland, Seirra Leone, Senegal, Serbia, Seychelles, Sierra Leone, Singapore, Slovakia, Slovenia, Solomon Islands, Somalia, South Korea, South Sudan, South-Africa, Spain, Sri Lanka, Sudan, Suriname, Swaziland, Sweden, Switzerland, Syrian Arab Republic, Taiwan, Tajikistan, Tanzania, Thailand, Timor-Leste, Togo, Tokelau, Trinidad-Tobago, Tunisia, Turkey, Tuvalu, Uganda, Ukraine, United Arab Emirates, United Kingdom, United States, Uruguay, Uzbekistan, Vanuatu, Vatican City, Venezuela, Vietnam, Wales, Yemen, Zambia, Zimbabwe

Study Fields

Aerospace Engineering, CFD, Mechanical Engineering

GPA / Grade

GPA 3.3

Languages

DuoLingo English Test 120, ELLT 7, IELTS 6.5, PTE A 67, TOEFL iBT 92

Tests

Study Levels

Doctoral, PhD

Total Scholarships

Transcripts

Yes

Degrees

Yes

Essay

Yes

Passport ID

Recommendation Letters

Yes (2)

Result Date

Program Start

September 2026

Tuition Fee

Covered

Living Allowance

Yes

Travel Allowance

Research Grant

Health Insurance

Visa Assistance

📞 Contact Information

Call if you want a quick answer, send an email for detailed questions, or follow the university’s social channels to keep an eye on updates and reminders. Use whatever fits your style and timezone.

Scholarship Summary

Award Amount
Deadline30 Jun, 2026
LevelDoctoral, PhD
InstitutionUniversity of Southampton
CountryUnited Kingdom
ModeOnline
TypeFully funded

Apply Now

The Modelling of Liquid-Fuelled Rotating Detonation Engines for Gas-Turbine Applications Scholarship is a fully funded PhD research opportunity offered by the University of Southampton in the United Kingdom. The project focuses on improving next-generation gas turbine efficiency by replacing conventional combustion systems with rotating detonation engines (RDEs). These systems use pressure-gain combustion instead of constant-pressure combustion. As a result, they can significantly increase propulsion efficiency in aerospace and power-generation applications.

Background and Purpose

The research develops advanced computational fluid dynamics (CFD) models for liquid-fuelled RDEs. In particular, it extends the university’s in-house AMROC simulation framework. Researchers incorporate two-phase flow physics, including spray combustion, droplet evaporation, and hydrocarbon chemical kinetics. Moreover, these improvements allow accurate modelling of liquid fuel behaviour in detonation-driven environments, which remains a major limitation in current simulation tools.

In addition, the project runs large-scale high-performance simulations of rotating detonation waves in both two-dimensional and three-dimensional configurations. After model development and validation, the upgraded solver applies to realistic gas-turbine conditions. These include kerosene–air mixtures relevant to industrial aero-engine systems. Consequently, the work connects directly to technologies used in modern propulsion research and engine design, including those developed by Rolls-Royce Plc.

Modelling of Liquid-Fuelled Rotating Detonation Engines for Gas-Turbine Applications Scholarship Benefits

The scholarship operates under the EPSRC Industrial Doctoral Landscape Award (IDLA) framework, supported by EPSRC. It provides full funding for doctoral research, including tuition support and financial maintenance. In addition, students gain access to a strong industrial research environment and advanced computational resources at the University of Southampton. Furthermore, the program includes training in combustion modelling, numerical methods, high-performance computing, and aerospace propulsion systems.

Eligibility Criteria

Applicants must hold a strong academic background in mechanical engineering, aerospace engineering, applied mathematics, or related disciplines. They should demonstrate knowledge of fluid dynamics, combustion, or numerical simulation. Moreover, experience in programming and high-performance computing will strengthen an application.

Modelling of Liquid-Fuelled Rotating Detonation Engines for Gas-Turbine Applications Scholarship Application Process

Candidates must apply through the University of Southampton’s postgraduate research portal. They should submit academic transcripts, a CV, and supporting documents. In addition, shortlisted applicants may be invited for an interview to assess their technical knowledge and research potential.

Opportunities for Scholars

This PhD provides strong opportunities in advanced propulsion research and computational combustion modelling. Students develop expertise in rotating detonation systems, CFD development, and multiphase flow simulation. Additionally, collaboration with industry partners enhances exposure to real-world gas-turbine engineering challenges. Consequently, graduates can pursue careers in aerospace research, propulsion industries, and advanced energy systems development.

Frequently Asked Questions (FAQs)

What is the main aim of this PhD project?

The project aims to extend an in-house RDE simulation tool by adding two-phase flow and spray combustion modelling to accurately predict the performance of liquid-fuelled rotating detonation engines.

What methods and tools are used in this PhD?

The research uses massively parallel computational fluid dynamics (CFD), Lagrangian droplet tracking, evaporation models, reduced chemical kinetics, and enhanced spray breakup modelling within the AMROC simulation framework.

What is the final goal of the simulations?

After validation, the model will be used to simulate realistic RDE combustion chambers operating under conditions similar to kerosene-fuelled Rolls-Royce jet engines to evaluate efficiency improvements from pressure-gain combustion.