Development of flow and heat transfer models for the carbon fiber rope in nozzle joints of the space Shuttle Reusable Solid Rocket Motor-Reference-Cited by-同舟云学术

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Development of flow and heat transfer models for the carbon fiber rope in nozzle joints of the space Shuttle Reusable Solid Rocket Motor

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Wang Qunzhen¹,Ewing Mark¹,Mathias Ed¹,Smith Cory¹,Heman Joe¹

Affiliation:

1. ATK Thiokol Propulsion, Brigham City, UT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3441

Reference46 articles.

1. (8) Rec= 20901^ | (9)

2. f F Val = 0.758- 0.0109 -

3. Flam=1.5-1.9r+1.96r2-0.71r3(16) for laminar flow and

4. Nu= 1.18135+ 2.30595r0403245(24) where the ratio r is defined in equation (18). For turbulent flow, the Nusselt number is calculated using the following empirical correlation

5. /PrRe max(pr2/3,(l.07-12.7>///8(Pr2/3-l)J&L

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