Autor: |
Soo Hyung Park, Jang-Hyuk Kwon, Yung-Hoon Yu |
Rok vydání: |
2006 |
Předmět: |
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Zdroj: |
Journal of the Korean Society for Aeronautical & Space Sciences. 34:1-8 |
ISSN: |
1225-1348 |
DOI: |
10.5139/jksas.2006.34.11.001 |
Popis: |
A steady prediction method is presented to compute dynamic damping coefficients for axisymmetric projectiles. Viscous flow analysis is essential to the steady method using a zero-spin coning motion in the inertial coordinate frame. The present method is applied to compute the pitching moment and the pitch-damping moment coefficients for the Army-Navy Spinning Rocket. The results are in good agreement with the parabolized Navier-Stokes data, range data, and unsteady prediction data. Predictions for Secant-Ogive-Cylinder configurations are performed to investigate effects of afterbody geometries. To investigate the geometrical effect and flow physics, the longitudinal developments of the coefficients are examined in detail. |
Databáze: |
OpenAIRE |
Externí odkaz: |
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