Navier-Stokes Investigation on Reacting Flow Field of HTPB/O2 Hybrid Motor and Regression Rate Evaluation-Reference-Cited by-同舟云学术

Navier-Stokes Investigation on Reacting Flow Field of HTPB/O2 Hybrid Motor and Regression Rate Evaluation

Published:2003-06-26 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Serin Nadir¹,Gogus Yalcin²

Affiliation:

1. Tubitak-Sage

2. Middle East Technical University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4462

Reference10 articles.

1. Serin, N., Measurement and Simulation of Regression Rate and Development of a Design Code for Hybrid Rocket Motors, Ph.D. Thesis in theMiddle East Technical University, Ankara, 2001.

2. Regression Rate Behavior of Hybrid Rocket Solid Fuels

3. Spectral and total emissivity of water vapor and carbon dioxide

4. A Fast Computer Code for Hybrid Motor Design, Eulec, and Results Obtained for HTPB/O2 Combination

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