Performance analysis of dual-duct rotating detonation aero-turbine engine

Published 2019 View Full Article

  1. Home
  2. Publications
  3. Publication Search
  4. Publication Details
Title
Performance analysis of dual-duct rotating detonation aero-turbine engine
Authors
Keywords
Rotating detonation aero-turbine engine, Detonation based propulsion, Thermodynamic analysis, Overall performance, Optimum compressor pressure ratios
Journal
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 92, Issue -, Pages 806-819
Publisher
Elsevier BV
Online
2019-07-09
DOI
10.1016/j.ast.2019.07.011

Ask authors/readers for more resources

Protocol

Community support

Reagent

Community support

Reprint

Contact the author

Create your own webinar

Interested in hosting your own webinar? Check the schedule and propose your idea to the Peeref Content Team.

Create Now

Become a Peeref-certified reviewer

The Peeref Institute provides free reviewer training that teaches the core competencies of the academic peer review process.

Get Started
Webinars Posters Questions Hubs Funding Journals Articles Connect Collections Reviewers About Us FAQs Mobile App Privacy Policy Terms of Use
© Peeref 2019-2024. All rights reserved.