Heterogeneous Combustion Studies on Polystyrene and Oxygen Styrene Copolymer
Author:
Affiliation:
1. University of Gorakhpur, Gorakhpur (U.P.) India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49451
Reference11 articles.
1. Hybrid Rocket Theory and Design
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4. TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKET
5. Holman, J. P., Heat Transfer, McGraw-Hill, New York, 1963, pp.114-116.
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