Characterization And Control Of Vortex Breakdown Over A Delta Wing At High Angles Of Attack

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Characterization and Control of Vortex Breakdown Over a Delta Wing at High Angles of Attack
Language: en
Pages: 380
Authors: Anthony M. Mitchell
Categories:
Type: BOOK - Published: 2000-08-01 - Publisher:

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Demands for more maneuverable and stealthy air vehicles have encouraged the development of new control concepts for separated flows. The goalof this research is
Computational Fluid Dynamics Investigation of Vortex Breakdown for a Delta Wing at High Angle of Attack
Language: en
Pages: 172
Authors: Jacob A. Freeman
Categories: Delta wing airplanes
Type: BOOK - Published: 2003-03-01 - Publisher:

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Using the commercially available FLUENT 3-D flow field solver, this research effort investigated vortex breakdown over a delta wing at high angle of attack (a)
Velocity Field Over Delta Wings at High Angles of Attack
Language: en
Pages: 66
Authors: Devin O. O'Dowd
Categories: Airplanes
Type: BOOK - Published: 1999-02-01 - Publisher:

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The study of vortex breakdown over delta wings at high angles of attack (AOA) has been an interest to researchers, mathematicians, and aircraft designers for de
High Angle of Attack Aerodynamics
Language: en
Pages: 408
Authors: Josef Rom
Categories: Science
Type: BOOK - Published: 2012-12-06 - Publisher: Springer Science & Business Media

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The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the
Structure and Control of Three-Dimensional Unsteady Flow in Delta Wings at High Angle-of-Attack
Language: en
Pages: 8
Authors:
Categories:
Type: BOOK - Published: 1995 - Publisher:

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This program has focused on the instantaneous flow structure generated by controlled motion of wings in the pitching and rolling modes, as well as application o