List of Journals    /    Call For Papers    /    Subscriptions    /    Login
 
 
 
 
 SEARCH
By Author By Title
 
 
ABOUT CSC
 About CSC Journals
 CSC Journals Objectives
 List of Journals
 CALL FOR PAPERS
 Call For Papers CFP
 Special Issue CFP
AUTHOR GUIDELINES
 Submission Guidelines
 Peer Review Process
 Helpful Hints For Getting Published
 Plagiarism Policies
 Abstracting & Indexing
 Open Access Policy
 Submit Manuscript
 FOR REVIEWERS
 Reviewer Guidelines
 FOR EDITORIAL
 Editor Guidelines
 Join Us As Editor
 Launch Special Issue
 Suggest New Journal
 CSC LIBRARY
 Browse CSC Library
 Open Access Policy
  SERVICES
 Conference Partnership Program (CPP)
 Abstracting & Indexing
 SUBSCRIPTIONS
 Subscriptions
 Discounted Packages
 Archival Subscriptions
 How to Subscribe
 Librarians
 Subscriptions Agents
 Order Form
 DOWNLOADS
 
 
 
 
Applications of Circulation Control, Yesterday and Today
Full text
 PDF(784.6KB)
Source 
International Journal of Engineering (IJE)
Table of Contents
Download Complete Issue    PDF(4.8MB)
Volume:  4    Issue:  5
Pages:  321-462
Publication Date:   December 2010
ISSN (Online): 1985-2312
Pages 
411 - 429
Author(s)  
Jonathan Kweder - United States of America
Chad Panther - United States of America
James Smith - United States of America
 
Published Date   
20-12-2010 
Publisher 
CSC Journals, Kuala Lumpur, Malaysia
ADDITIONAL INFORMATION
Keywords   Abstract   References   Cited by   Related Articles   Collaborative Colleague
 
KEYWORDS:   Circulation Control, Lift Augmentation, Drag Reduction 
 
 
This Manuscript is indexed in the following databases/websites:-
1. PDFCAST
2. Directory of Open Access Journals (DOAJ)
3. Scribd
4. Docstoc
5. Libsearch
 
 
Circulation control, an aerodynamic method of changing the properties of an airfoil, such as lift, camber and angle of attack, has been used in several unique ways since its inception, as an enhancement to fixed wing aircraft, in the 1960’s. Early in the research venture, this technology was used on the main wing of an aircraft in conjunction with a Coandă surface, such as a rounded trailing edge or a deployable flap. Research during this time proved to be the foundation of the circulation control technology and showed that small amounts of exit jet velocity could have a large impact on the aerodynamics of an airfoil. In the 1970’s the inspirations that drove circulation control research changed from design work to optimization of the parameters which were found to have the most effect on circulation control. These studies included slot placement, favorable momentum coefficient, and pressurization benefits and determents. This research period also allowed for expansion of the uses of circulation control to submarine/hydrodynamic and rotary wing applications. Newest research has brought on several propeller driven applications and the recent push for efficient renewable research has allowed circulation control research technologies to evolve into use in wind turbine and water turbine applications. The idea being that with circulation control the turbine can adapt easier to the changing wind velocity and direction and ultimately capture more power than an un-augmented turbine. As with most new and novel technologies there is a process and time delay associated with their development and ultimate application. For some technologies the market, or the supporting hardware, are lacking and sometimes the technology has strong advocacies for yet to be fulfilled expectations. In most of these cases a strong idea will re-surface repeatedly until the art has matured, or the better solution is found. This paper will focus on the previously developed circulation control research, from its beginnings, as used on fixed wing aircraft, following the progression, as this technology evolved through the past five decades, to its now more widely considered potential. 
 
 
 
1 Abbott, I.H., Von Doenhoff, A. E., Theory of Wing Sections, Dover Publications, Inc, New York, NY, 1959.
2 Abramson, J. “Two-Dimensional Subsonic Wind Tunnel Evaluation of a 20-Percent-Thick Circulation Controlled Airfoil.” David W. Taylor Naval Ship Research Center, Bethesda, MD, 1975.
3 Abramson, J. “Characteristics of a Cambered Circulation Control Airfoil Having Both Upper and Lower Surface Trailing Edge Slots.” Naval Surface Warfare Center – Carderock Division, Bethesda, MD, 2004
4 Ambrosiani, J.P., “Analysis of a Circulation Controlled Elliptical Airfoil,” Doctorate of Philosophy Dissertation, Department of Mechanical and Aerospace Engineering, West Virginia University, Morgantown, WV, 1971.
5 Angle II, G.M., Huebsch, W.W., Prucz, J.C., Smith, J.E. “Circulation Controlled, Fixed-Root Helicopter Concept.” American Helicopter Society 62 nd Annual Forum, Phoenix, AZ, 2006.
6 Angle II, G.M., “Aerodynamic Benefits of Near-Surface-Actuated Circulation Control Blowing Slots for Rotorcraft Use,” Doctorate of Philosophy Dissertation, Department of Aerospace Engineering, West Virginia University, Morgantown, WV, 2008.
7 Ashworth, J.C. “An Experiment Investigation of a Circulation Controlled Shrouded Propeller.” Master of Science Thesis, Department of Mechanical and Aerospace Engineering, West Virginia University, Morgantown, WV, 1973.
8 Bons, J.P., Sondergaard, R.B., Rivir, R.B., The Fluid Dynamics of LPT Blade Separation Control Using Pulsed Jets.” Journal of Turbomachinery, Vol. 124, Issue 1, 2002.
9 Churchill, R.A. “Coand? Effect Jet Around a Cylinder with an Interacting Adjacent Surface,” Doctorate of Philosophy Dissertation, Department of Aerospace Engineering, West Virginia University, Morgantown, WV, 1992.
10 Donnelly, M.J., Cutbirth, J.M., Rogers, E.O., Jessup, S.D., Park, J.T. “Hydrodynamic Performance of a Dual-Slotted Circulation Control Wing of Low Aspect Ratio,” Naval Surface Warfare Center, Carderock Division, Hydrodynamics Department Report, TR-2006-031, Bethesda, MD, 2006.
11 Englar, R. J., “Two-Dimensional Subsonic Wind Tunnel Tests of Two 15-Percent Thick Circulation Control Airfoils,” David W. Taylor Naval Ship Research and Development Center Technical Note AL- 211, Washington, DC, 1971.
12 Englar, R.J., Williams, R.M., “Design of a Circulation Control Stern Plane for Submarine Applications.” David W. Taylor Naval ship Research and Development Center, Bethesda, MD, 1971.
13 Englar, R.J., Williams, R.M. “Test Techniques for High Lift, Two-Dimensional Airfoils with Boundary Layer and Circulation Control for Application to Rotary Wing Aircraft.” Canadian Aeronautics and Space Journal, Vol. 19, No. 3, 1973.
14 Englar, R.J., “Subsonic Two-Dimensional Wind Tunnel Investigation of the High Lift Capability of Circulation Control Wing Sections.” David W. Taylor Naval ship Research and Development Center, Bathesda, MD, 1975.
15 Englar, R.J., “Experimental Investigation of the High Velocity Coand? Wall Jet Applied to Bluff Trailing Edge Circulation Control Airfoils,” David W. Taylor Naval Research and Development Center Report 4708, September 1975.
16 Englar, R.J., “Development of the A-6/Circulation Control Wing Flight Demonstrator Configuration.” David W. Taylor Naval Ship Research and Development Center, Bethesda, MD, 1979.
17 Englar, R.J., Nichols, J.H., Harris, M.J., Eppel, J.C., Shovlin, M.D., “Circulation Control Technology Applied to Propulsive High Lift Systems.” Society of Automotive Engineers, Aerospace Congress and Exposition, Long Beach, CA, 1984.
18 Englar, R.J., “The Application of Circulation control Pneumatic Technology to Powered-lift STOL Aircraft.” Advanced Flight Systems Department, Lockheed Aeronautical Systems Company, Marietta, GA, 1987.
19 Englar, R.J., Smith, M.J., Neibur, C.S., Gregory, S.D., “Development of Pneumatic Aerodynamic Concepts for Control of Lift, Drag and Moment plus Lateral/Directional Stability of Automotive Vehicles.” Georgia Tech Research Institute Journal of Technology, Atlanta, GA, 1996.
20 Englar, R.J., “Overview of Circulation Control Pneumatic Aerodynamics: Blown force and Moment Augmentation and Modification as Applied Primarily to Fixed Wing Aircraft,” Proceedings of the 2004 NASA/ONR Circulation Control Workshop, NASA CP-2005-213509, Pages 23-66, 2005.
21 Englar, R.J., “Pneumatic Aerodynamic Technology to Improve Performance of Automotive Vehicles.” American Institute of Aeronautics and Astronautics, Inc. 2005.
22 Englar, R.J., Jones, G.S., Allan, B.G., Lin, J.C., “2-D Circulation Control Airfoil Benchmark Experiments Intended for CFD Code Validation.” American Institute of Aeronautics and Astronautics, 47 th Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, FL, 2009.
23 Englar, R.J., “The Application of Pneumatic Aerodynamic Technology to Improve Performance and Control of Advanced Automotive Vehicles.” Georgia Tech research institute: Aerospace, Transportation and Advanced Systems Lab, Atlanta, GA, 2009.
24 Franke, M.E., Harvell, J.K., “Wind Tunnel Studies of Circulation Control Elliptical Airfoils.” Air Force Institute of Technology, Tech #N88-17598, Wright-Patterson Air Force Base, Dayton, OH, 1987
25 Gibbs, E.H., “Analysis of Circulation Controlled Airfoils,” Doctorate of Philosophy Dissertation, Department of Mechanical and Aerospace Engineering, West Virginia University, Morgantown, WV, 1975.
26 ] Harness, G.S., “An Experimental Investigation of a Circulation Controlled Cambered Elliptical Airfoil,” Master of Science Thesis, Department of Aerospace Engineering, West Virginia University, Morgantown, WV, 1970.
27 Holt, D.J., “Circulation Controlled Airfoil with Pulsed Flow.” Master of Science Thesis Department of Mechanical and Aerospace Engineering, West Virginia University, Morgantown, WV, 1972.
28 Kind, R.J., Maul, D.J., “An Experimental Investigation of a Low-Speed Circulation-Controlled Aerofoil,” The Aeronautical Quarterly, Vol. XIX, May, 1968.
29 Kondor, S., Englar, R.J., Moore, M. “Experimental Investigation of Circulation Control on a Shrouded Fan,” American Institute of Aeronautics and Astronautics, 21 st Applied Aerodynamics Conference, Orlando, FL, 2003.
30 Loth, J.L., Fanucci, J.B., Roberts, S.C., “Flight Performance of a Circulation Controlled STOL Aircraft.” Journal of Aircraft, American Institute of Aeronautics and Astronautics, Vol. 13, No. 3, 1976
31 Loth, J.L., Boasson, M. “Circulation Control STOL Wing Optimization,
32 ] Loth, J.L., Funk, M.S., “Thrust Savings Limitations with Blown high Lift Wings.” AIAA/AHS/ASEE Aircraft Design, Systems and Operations Meeting, St. Louis, MO, 1987.
33 ] Loth, J.L, Browning, P., Posada, A., “Engineering Solutions for Circulation Control Applications.” Society of Automotive Engineers, AeroTech Congress and Exhibition, Grapevine, TX, 2005.
34 ] Maskell, E.C., Spence D.A., “A Theory of the Jet Flap in Three Dimensions,” Proceedings of the Royal Society of London, A Mathematical and Physical Sciences Series, Vol. 251, No. 1266, 1959.
35 Mosher, M., “Acoustics of Rotors Utilizing Circulation Control.” American Institute of Aeronautics and Astronautics Journal of Aircraft, Vol. 20, No. 11, 1981.
36 Myer, D.P., “An Investigation of a Circulation Controlled Cambered Elliptical Airfoil with a Rounded Trailing Edge,” Master of Science Thesis, Aerospace Engineering Department, West Virginia University, Morgantown, WV, 1972.
37 Naqvi, M.A., “Prediction of Circulation Control Performance Characteristics for Super STOL& STOL Applications.” Doctorate of Philosophy Dissertation, Georgia Institute of Technology, 2006.
38 Newman, B.G. “The Deflexion of Plane Jets by Adjacent Boundaries – Coand? Effect,” Boundary Layer Flow Control, Pergamon Press, Vol. 1, 1961.
39 Novak, C.J., Cornelius, K.C., Roads, R.K., “Experimental Investigations of the Circular Wall Jet on a Circulation Control Airfoil.” American Institute for Aeronautics and Astronautics, 25 th Aerospace Sciences Meeting, Reno, NV, 1987.
40 Ottensoser, J. “Two-Dimensional Subsonic Evaluation of a 15-Percent Thick Circulation Control Airfoil with Slots at Leading and Trailing Edges.” David W. Taylor Naval Ship Research and Development Center, Bethesda, MD, 1974.
41 Rae Jr., W.H., Shindo, S., “Comments on V/STOL Wind Tunnel Data at Low Forward Speeds.” Washington University, Seattle, WA, 1969.
42 Reader, K.R., Wilkerson, J.B., “Circulation Control Applied to a High Speed Helicopter Rotor.” David W. Taylor Naval Ship Research and Development Center, Bethesda, MD, 1976.
43 Rodman, L.C., Wood, N.J., “Verification of Performance for a Low-Speed 15% Elliptical Circulation Control Airfoil,” Stanford University, Stanford CA, 1986.
44 Rogers, E.O., Donnelly, M.J., “Characteristics of a Dual-Slotted Circulation Control Wing of Low Aspect Ratio Intended for Naval Hydrodynamic Applications.” American Institute of Aeronautics and Astronautics, 42 nd Aerospace Sciences Meeting, Reno, NV, 2004
45 Seif, M.S, Tavakoli, M.T., “New Technologies for Reducing Fuel Consumption in Marine Vehicles,” XVI SORTA Symposium, Croatia, 2004.
46 Smith, J.E., Loth, J.L., Craven, R.P.M., Bond, R., “Piezoelectric Actuators for Circulation Controlled Rotorcraft,” US Patent 6,425,553 B1. 2002.
47 Songlin, Z., Zianfu, W. “Experimental Investigation of a High-Lift Rudder-Circulation Control Rudder.” Journal of International Shipbuilding Progress, Vol. 43, No. 436, 1996
48 Tai, J.C., Mavris, D.N., Schrage, D.P., “An Assessment of a Reaction Driven Stopped Rotor/Wing Using Circulation Control in Forward Flight.” American Institute of Aeronautics and Astronautics, World Aviation Congress, Los Angeles, CA, 1996.
49 Theodorsen, T., “Theory of Wing Sections of Arbitrary Shape,” NACA-TR-411, 1931
50 Tongcitpakdee, C., “Computational Studies of the Effects of Active and Passive Circulation Enhancement Concepts on Wind Turbine Performance.” Doctorate of Philosophy Dissertation, School of Aerospace Engineering, Georgia Institute of Technology, 2007.
51 Tongcitpakdee, C., Benianirat, S., Sankar, L.N., “Numerical Studies of the Effects of Active and Passive Circulation Enhancement Concepts on Wind Turbine Performance.” Journal of Solar Energy Engineering, American Society of Mechanical Engineers, Vol. 128, No. 4, 2006.
52 ] Wood, N.J., “The Aerodynamics of Circulation Control Aerofoils.” Joint Institute for Aeronautics and Astronautics, Stanford University, Stanford, CA, 1986.
53 Ward, C.C., “Circulation Control technique on a Marine Propeller Duct.” Master of Science Thesis, department of Naval Architecture and Marine Engineering, University of Strathclyde, Glasgow, U.K., 2006.
54 Wilhelm, J.P., Pertl, E.D., Pertl, F.A., Smith, J.E. “Performance Predictions of a Circulation Controlled-Vertical Axis Wind Turbine with Solidity Control,” American Society of Mechanical Engineers, Energy Sustainability Conference, San Francisco, CA, 2009.
55 ] Wilhelm, J.P., Panther, C.C., Pertl, F.A., Smith, J.E. “Vortex analytical Model of a Circulation Controlled Vertical Axis Wind Turbine,” American Society of Mechanical Engineers, Energy Sustainability Conference, San Francisco, CA, 2009.
56 ] Wilkerson, J.B., Reader, K.R., Linck, D.W., “The Application of Circulation Control Aerodynamics to a Helicopter Rotor Model.” American Helicopter Society, 29 th Annual Forum, Washington, D.C., 1973.
57 Williams, R.M., “Some Aspects on Rotor Circulation Control.” CAL/AVLABS 3 rd Symposium of Rotary Wing and V/STOL Aircraft, Buffalo, NY, 1969.
58 Wood, N. J., “The Aerodynamics of Circulation Control Aerofoils,” Stanford University Technical Report (SU-JIAA TR-41), Stanford, CA, 1981.
 
 
 
 
 
 
1 MENDELEY
 
2 CORE
 
 
 
Jonathan Kweder : Colleagues
Chad Panther : Colleagues
James Smith : Colleagues  
 
 
 
  Untitled Document
 
Copyrights (c) 2012 Computer Science Journals. All rights reserved.
Best viewed at 1152 x 864 resolution. Microsoft Internet Explorer.
 
  
 
Copyrights & Usage: Articles published by CSC Journals are Open Access. Permission to copy and distribute any other content, images, animation and other parts of this website is prohibited. CSC Journals has the rights to take action against individual/group if they are found victim of copying these parts of the website.