Experimental Closed-Loop Flow Control of a von Kármán Ogive at High Incidence-Reference-Cited by-同舟云学术

Experimental Closed-Loop Flow Control of a von Kármán Ogive at High Incidence

Published:2014-12 Issue:12 Volume:52 Page:2891-2898
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Fagley Casey¹,Porter Chris¹,McLaughlin Thomas¹

Affiliation:

1. Department of Aeronautics, U.S. Air Force Academy, Colorado Springs, Colorado 80840

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053012

Reference26 articles.

1. A physical model of asymmetric vortices flow structure in regular state over slender body at high angle of attack

2. Unsteady flow around an ogive cylinder

3. KeenerE. R.ChapmanG. T. “Side Forces on a Tangent Ogive Forebody with a Fineness Ratio of 3.5 at High Angles of Attack and Mach Numbers from 0.1 to 0.7,” NASA TM-X-3437, 1977.

4. BridgesD. H. “The Asymmetric Vortex Wake Problem: Asking the Right Question,” AIAA Paper 2006-3553, 2006.

5. Recent progress on the study of asymmetric vortex flow over slender bodies

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