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Analysis of transverse force in the case of flow about bodies of revolution at high angle of attack
- Authors: Gumerov A.V.1, Gumerova L.V.1, Balzannikova Y.M.2
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Affiliations:
- Samara Space Rocket Centre “TsSKB-Progress”
- Samara State University of Civil Architecture and Engineering
- Issue: Vol 8, No 1 (2009)
- Pages: 14-23
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/629
- DOI: https://doi.org/10.18287/2541-7533-2009-0-1(17)-14-23
- ID: 629
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Abstract
The paper analyses cross separation flow about an impulsively started circular cylinder in a non-viscous non-compressible medium by the vortex method. The impact of viscosity on resistance is expressed through the circulation of vortices formed behind the cylinder. By analogy the computation of plane flow is reduced to the computation of transverse force when a body of revolution moves at an angle of attack.
About the authors
A. V. Gumerov
Samara Space Rocket Centre “TsSKB-Progress”
Author for correspondence.
Email: vest@ssau.ru
Russian Federation
L. V. Gumerova
Samara Space Rocket Centre “TsSKB-Progress”
Email: vest@ssau.ru
Russian Federation
Ye. M. Balzannikova
Samara State University of Civil Architecture and Engineering
Email: vest@ssau.ru
Russian Federation
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