Effect of multiple rings on side force over an ogive-cylinder body at subsonic speed
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference20 articles.
1. Allen HJ, Perkins EW. Characteristics of flow over inclined bodies of revolution. Washington, D.C.: NASA; 1951. Report No.: NACA RM A50L07.
2. Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream;Lamont;J Fluid Mech,1976
3. Pressures around an inclined ogive-cylinder with laminar, transitional, or turbulent separation;Lamont;AIAA J,1982
4. Asymmetric vortices on slender body of revolution;Zilliac;AIAA J,1991
5. Dexter PC, Hunt BL. The effects of roll angle on the flow over a slender body of revolution at high angles of attack. Reston: AIAA; 1981. Report No.: AIAA-1981-0358.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Research on the characteristics of the leeward vortex flow field on a blunt-headed rotating body at high angles of attack;AIP Advances;2022-06-01
2. Determining the side force appearance and its magnitude over a slender body at high angle of attack;Thermophysics and Aeromechanics;2021-11
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