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Article
Methodology for Performance Analysis of Aerospace Vehicles Using the Laws of Thermodynamics
Journal of Aircraft
  • David W. Riggins, Missouri University of Science and Technology
  • Trent M. Taylor
  • David J. Moorhouse
Abstract

Theory, methodology, and example applications are developed and shown for the systematic analysis of overall vehicle forces in terms of irreversibility and heat. The methodology presented involves analyzing and deconstructing vehicle forces using individual stream tubes as components within the overall fluid control volume in which the vehicle is embedded. This provides the capability for the complete fluid/thermodynamic “audit” of vehicle performance in terms of irreversibility, combustion (heating), and fluid dynamic flow turning and area change. Sample results are shown for a simplified hypersonic vehicle configuration modeled with constant specific heats and Rayleigh heating. The role of overall entropy generation and wake mixing processes in the production of vehicle forces in atmospheric flight is next discussed and clarified. Specifically, the direct analytical relationship between entropy, wake mixing processes, and overall force production for the vehicle is developed from fundamental considerations of the global control volume with inclusion of the wake in the analysis. This analysis is demonstrated using the same simplified high-speed configuration and is finally developed for the completely general problem of an aerospace vehicle with variable specific heats, thermal loading, variable composition, fuel injection, and chemical reaction.

Department(s)
Mechanical and Aerospace Engineering
Keywords and Phrases
  • Aerospace Vehicles,
  • Rayleigh Heating,
  • Thermodynamics,
  • Combustion,
  • Entropy Generation,
  • Fuel Injection,
  • Stream Tubes,
  • Thermal Loading
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2006 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
1-1-2006
Publication Date
01 Jan 2006
Citation Information
David W. Riggins, Trent M. Taylor and David J. Moorhouse. "Methodology for Performance Analysis of Aerospace Vehicles Using the Laws of Thermodynamics" Journal of Aircraft (2006) ISSN: 0021-8669
Available at: http://works.bepress.com/david-riggins/21/