Abstract
A wind tunnel test is designed to study aerodynamic effects of one individual rocket with deflectable nose. The test measures pressure with U-bend tube which is cost effective. Using rubber tubes in different lengths to measure pressure distributions of a flat-plate, and calculating how rubber tube affects the measurement, in order to modify the measured surface pressure of the nose. The surface pressure varies on different points while yawing angle and attack angle changes, the changing regularity could provide data for following numerical simulation and trajectory control.
| Original language | English |
|---|---|
| Title of host publication | Applied Materials and Technologies for Modern Manufacturing |
| Pages | 2063-2067 |
| Number of pages | 5 |
| DOIs | |
| Publication status | Published - 2013 |
| Event | 3rd International Conference on Applied Mechanics, Materials and Manufacturing, ICAMMM 2013 - Dalian, China Duration: 24 Aug 2013 → 25 Aug 2013 |
Publication series
| Name | Applied Mechanics and Materials |
|---|---|
| Volume | 423-426 |
| ISSN (Print) | 1660-9336 |
| ISSN (Electronic) | 1662-7482 |
Conference
| Conference | 3rd International Conference on Applied Mechanics, Materials and Manufacturing, ICAMMM 2013 |
|---|---|
| Country/Territory | China |
| City | Dalian |
| Period | 24/08/13 → 25/08/13 |
Keywords
- Aerodynamic effect
- Deflectable nose
- Wind tunnel
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Zhang, B., Wang, S. S., Cao, M. Y., & Xu, Y. X. (2013). Design and research of wind tunnel test for deflectable nose. In Applied Materials and Technologies for Modern Manufacturing (pp. 2063-2067). (Applied Mechanics and Materials; Vol. 423-426). https://doi.org/10.4028/www.scientific.net/AMM.423-426.2063