A Fast Computer Code for Hybrid Motor Design, Eulec, and Results Obtained for HTPB/O2 Combination-Reference-Cited by-同舟云学术

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

Published:2003-06-26 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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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/10.2514/6.2003-4747

Reference14 articles.

1. Regression Rate Behavior of Hybrid Rocket Solid Fuels

2. 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.

3. Serin, N., Gogus, Y. "Navier-Stokes Investigation on Reacting Flow Field of HTPB/O2 Hybrid Motor and RegressionRate", AIAA-2003-4462.

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