Crossmark

Trailing Edge Modifications for Enhanced Jet Decay: The Effect of Groove Depth on Supersonic Rectangular Nozzles

Published Online: 2026-02-05

Published Print: 2025-12

Authors

Hannah R, R. S.

Wessley, G. J. J.
License Information

Text and Data Mining valid from 2025-12-01

Version of Record valid from 2025-12-01
More Information

Article History

Received: 8 July 2025

Revised: 27 October 2025

Accepted: 28 October 2025

First Online: 5 February 2026

CONFLICT OF INTEREST

: The authors of this work declare that they have no conflicts of interest.

Document is current