Nozzle guide vane integration into rotating detonation engine

Authors

• Nick D. DeBarmore, Air Force Institute of Technology
• Paul I. King, Air Force Institute of Technology
• Frederick R. Schauer, Air Force Institute of Technology
• 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 N. DeBarmore was an AFIT graduate student at the time of this conference. (AFIT-ENY-13-M-09, March 2013 graduate)

DOI

10.2514/6.2013-1030

Source Publication

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

Recommended Citation

DeBarmore, N. D., King, P. I., Schauer, F. R., & Hoke, J. L. (2013, January 7). Nozzle Guide Vane Integration into Rotating Detonation Engine. 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. https://doi.org/10.2514/6.2013-1030