Investigation of a circular planform wing with tangential fluid ejection

Author:

Imber Robin1,Rogers Ernest1

Affiliation:

1. U.S. Navy, Naval Surface Warfare Center, Bethesda, MD

Publisher

American Institute of Aeronautics and Astronautics

Reference20 articles.

1. Circulation control airfoils - Past, present, future

2. Circulation control wing model study

3. Control of vortical lift on delta wings by tangential leading-edge blowing

4. Demele, F.A.,and J.J.Brownson, "Subsonic Longitudinal Aerodynamic Characteristics of Disks with Elliptic Cross Sections and Thickness-Diameter Ratios from 0.225to 0.425,"NASA TechnicalNote D788,Apr.1961.

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1. Measurements of Midspan Flow Interactions of a Low-Aspect-Ratio Circulation Control Wing;Journal of Aircraft;2016-11

2. PIV Wake Measurements of a Low Aspect Ratio Circulation Control Wing with Spanwise Variation in Efflux;7th AIAA Flow Control Conference;2014-06-13

3. Mid-span PIV Measurements of a Low Aspect Ratio Circulation Control Wing;30th AIAA Applied Aerodynamics Conference;2012-06-25

4. Effects of Turbulence Modeling on RANS Simulations of Tip Vortices;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

5. Characteristics of a Dual-Slotted Circulation Control Wing of Low Aspect Ratio Intended for Naval Hydrodynamic Applications;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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