Ignition design for a rotating detonation engine

Authors

• Stephen J. Miller, Air Force Institute of Technology
• Paul I. King, Air Force Institute of Technology
• Frederick R. Schauer, Air Force Research Laboratory
• John L. Hoke, Innovative Scientific Solutions, Inc.

Document Type

Conference Proceeding

Publication Date

1-7-2013

Comments

The full conference paper is available from AIAA via subscription or purchase, using the DOI link on this page.

Co-author S. Miller was an AFIT graduate student at the time of this conference. (AFIT-ENY-13-M-23, March 2013 graduate)

DOI

10.2514/6.2013-1174

Source Publication

AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 51st

Recommended Citation

Miller, S., King, P. I., Schauer, F. R., & Hoke, J. L. (2013). Ignition Design For a Rotating Detonation Engine. 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA paper 2013-1174. https://doi.org/10.2514/6.2013-1174