Effects of radial curvature on net heat flux reduction in a film-cooled rocket

Authors

Jonathan F. McCall, Air Force Institute of Technology
Richard D. Branam, Air Force Institute of Technology

Document Type

Conference Proceeding

Publication Date

1-5-2009

Abstract

The effects of film cooling in a LOX/kerosene converging nozzle are analyzed.

Comments

Co-author J. McCall was an AFIT PhD student at the time of this paper. (AFIT-DS-ENY-09-D02, December 2009)

DOI

10.2514/6.2009-1586

Source Publication

AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 47th

Recommended Citation

McCall, J., & Branam, R. (2009, January 5). Effects of radial curvature on net heat flux reduction in a film-cooled rocket. 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, Orlando, Florida. https://doi.org/10.2514/6.2009-1586