Methodology for Performance Analysis of Aerospace Vehicles Using the Laws of Thermodynamics
Author:
Affiliation:
1. University of Missouri–Rolla, Rolla, Missouri 65409
2. U.S. Air Force Research Laboratory, Wright–Patterson AFB, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.16426
Reference18 articles.
1. Introduction: Exergy
2. Propulsive efficiency from an energy utilization standpoint
3. The Use of Stream Thrust Concepts for the Approximate Evaluation of Hypersonic Ramjet Engine Performance
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