Shock Structure Solution by Hybrid Flowfield Methods

Authors

Brook I. Bentley, Air Force Institute of Technology
Robert B. Greendyke, Air Force Institute of Technology

Document Type

Article

Publication Date

11-2012

Comments

This article is published as cited on this page, and is reachable by the DOI link below. A subscription is required for full article access.

Co-author B. Bentley was an AFIT PhD student at the time of this publication. (AFIT-ENY-DS-13-S-01, September 2013)

DOI

10.2514/1.A32179

Source Publication

Journal of Spacecraft and Rockets (ISSN 0022-4650)

Recommended Citation

Bentley, B. I., & Greendyke, R. B. (2012). Shock structure solution by hybrid flowfield methods. Journal of Spacecraft and Rockets, 49(6), 1058–1068. https://doi.org/10.2514/1.A32179