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Wright Field, Dayton, Ohio, Report No. F TR-2155-ND, April 3
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Alfred Jr., V.1
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Test Techniques for High Lift Two-Dimensional Airfoils with Boundary Layer and Circulation Control for Application to Rotary Wing Aircraft
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Canadian Aeronautics and Space Journal
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The Application of Circulation Control by Blowing to Helicopter Rotors
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Circulation Control Applied to A Circular Cylinder
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The Application of Circulation Control Aerodynamics to A Helicopter Rotor Model
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Englar, Robert J., "Experimental Investigation of the High Velocity Coanda Wall Jet Applied to Bluff Trailing Edge Circulation Control Airfoils," DTNSRDC Report 4708, Aero Report 1213, AD-A-019-417, September, 1975. Also M.S. Thesis, University of Maryland, Department of Aerospace Engineering, June 1973.
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Department of Aerospace Engineering
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Circulation Control Airfoils Past, Present, and Future
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X- Wing: A New Concept In Rotary VTOL
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Philadelphia, Pa., August
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AHA Symposium On Rotor Technology
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84877426168
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Potential Acoustic Benefits of Circulation Control Rotors
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NASA Langley Research Center, May
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Williams, R. M. and I. C. Cheeseman, "Potential Acoustic Benefits of Circulation Control Rotors," presented at AHS Meeting on Rotor Acoustics, NASA Langley Research Center, May, 1978.
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AHS Meeting On Rotor Acoustics
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Circulation Control for High Lift and Drag Generation on STOL Aircraft
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May
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Englar, Robert J., "Circulation Control for High Lift and Drag Generation on STOL Aircraft," AIAA Journal of Aircraft, Vol. 12, No. 5, pp. 457-463, May 1975.
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AIAA Journal of Aircraft
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AIAA Paper No. 77-578, June
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Englar, R.J., L. A. Trobaugh and R. A. Hemmerly, "Development of the Circulation Control Wing to Provide STOL Potential for High Performance Aircraft," AIAA Paper No. 77-578, June 6-8, 1977.
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Development of the Circulation Control Wing to Provide STOL Potential For High Performance Aircraft
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31
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Design of the Circulation Control Wing STOL Demonstrator Aircraft
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AIAA Paper No. 79-1842, August, 1979. Also published in, January
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Englar, R. J., R. A. Hemmerly, H. Moore, V. Seredinsky, W. G. Valckenaere, J. A. Jackson, Design of the Circulation Control Wing STOL Demonstrator Aircraft," AIAA Paper No. 79-1842, August, 1979. Also published in AIAA Journal of Aircraft, January, 1981.
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AIAA Journal of Aircraft
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Englar, R.J.1
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Moore, H.3
Seredinsky, V.4
Valckenaere, W.G.5
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Aviation Week and Space Technology
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Flight Performance of a Circulation Control STOL Aircraft
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AIAA Paper 74-994, April, 1974, March
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AIAA Journal of Aircraft
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Loth, J.L.1
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Development of Advanced Circulation Control Using High-Lift Airfoils
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AIAA Paper No. 83-1847,July 13-15, 1983. Also published, July
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Englar, R. J. and G. G. Huson, "Development of Advanced Circulation Control Using High-Lift Airfoils," AIAA Paper No. 83-1847,July 13-15, 1983. Also published AIAA Journal of Aircraft, pp.476-483, July, 1984.
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AIAA Journal of Aircraft
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Englar, R.J.1
Huson, G.G.2
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0028498946
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Development of Circulation Control Technology for Application to Advanced Subsonic Transport Aircraft
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AIAA Paper No. 93-0644, January 11-14, 1993. Also published as, September- October
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Englar, Robert J., Marilyn J. Smith, Sean M. Kelley and Richard C. Rover III, "Development of Circulation Control Technology for Application to Advanced Subsonic Transport Aircraft," AIAA Paper No. 93-0644, January 11-14, 1993. Also published as ALAA Journal of Aircraft, Vol. 31, No. 5, p. 1160-1177, September- October 1994.
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ALAA Journal of Aircraft
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Rover III, R.C.4
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0348097643
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AIAA Paper 97-0036, January
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Englar, Robert J., Niebur, Curt S., and Gregory, Scott D., "Pneumatic Lift and Control Surface Technology Applied to High Speed Civil Transport Configurations," AIAA Paper 97-0036, January, 1997.
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Pneumatic Lift and Control Surface Technology Applied to High Speed Civil Transport Configurations
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Englar, R.J.1
Niebur, C.S.2
Gregory, S.D.3
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84877454402
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GTRI Final Technical Report, A-5676, October 3
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Systems Analyses of Pneumatic Technology For High Speed Civil Transport Aircraft
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AIAA Paper No. 81-0151, January
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Nichols, J. H. Jr., R. J. Englar, M. J. Harris, and G. G. Huson, "Experimental Development of an Advanced Circulation Control Wing System for Navy STOL Aircraft," AIAA Paper No. 81-0151, January 12, 1981.
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Experimental Development of An Advanced Circulation Control Wing System For Navy STOL Aircraft
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Nichols Jr., J.H.1
Englar, R.J.2
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Huson, G.G.4
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45
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Development of the Circulation Control Wing/Upper Surface Blowing Powercd-Lift System for STOL Aircraft
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Paper No. ICAS-82-6.5.1, Seattle, August
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Harris, M. H., J. H. Nichols Jr., R. J. Englar, and G. G. Huson, "Development of the Circulation Control Wing/Upper Surface Blowing Powercd-Lift System for STOL Aircraft, Paper No. ICAS-82-6.5.1, in Proceedings of the ICAS/AIAA Aircraft Systems and Technology Conference, Seattle, August 22-27, 1982.
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Proceedings of the ICAS/AIAA Aircraft Systems and Technology Conference
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Englar, R. J., J. H. Nichols Jr., M. J. Harris, J. C. Eppel and M. D. Shovlin, "Circulation Control Technology Applied to Propulsive High Lift Systems," SAE Paper No. 841497, October, 1984.
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Circulation Control Technology Applied to Propulsive High Lift Systems
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Englar, R.J.1
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Harris, M.J.3
Eppel, J.C.4
Shovlin, M.D.5
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Aviation Week and Space Technology
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AIAA Paper No. 86-0476, January
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Englar, R. J., J. H. Nichols Jr., M. J. Harris, J. C. Eppel, and M. D. Shovlin, "Development of Pneumatic Thrust-Deflecting Powered-Lift Systems," AIAA Paper No. 86-0476, January, 1986.
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Development of Pneumatic Thrust-Deflecting Powered-Lift Systems
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Englar, R.J.1
Nichols Jr., J.H.2
Harris, M.J.3
Eppel, J.C.4
Shovlin, M.D.5
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50
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79952805679
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NASA TM 84232, July
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Eppel, J.C., M. D. Shovlin, D.N. Jaynes, R. J. Englar, and J. H. Nichols Jr., "Static Investigation of the CCW/USB Concept Applied to the Quiet Short-Haul Research Aircraft," NASA TM 84232, July, 1982.
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Static Investigation of the CCW/USB Concept Applied to The Quiet Short-Haul Research Aircraft
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Eppel, J.C.1
Shovlin, M.D.2
Jaynes, D.N.3
Englar, R.J.4
Nichols Jr., J.H.5
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51
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NASA Technical Paper 2684, January
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Shovlin, M.D., R. J. Englar, J. C. Eppel and J. H. Nichols Jr., "Large-Scale-Static Investigation of Circulation-Control-Wing Concepts Applied to Upper- Surface-BIowing Aircraft," NASA Technical Paper 2684, January, 1987.
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Large-Scale-Static Investigation of Circulation-Control-Wing Concepts Applied to Upper- Surface-BIowing Aircraft
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Englar, R.J.2
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In Proceedings of the Circulation Control Workshops 1986, NASA CP 2432, February
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Bevilaqua, P. M. and J. D. Lee, "Design of Supersonic Coanda Jet Nozzles," In Proceedings of the Circulation Control Workshops 1986, NASA CP 2432, pp. 289-312, February, 1986.
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Design of Supersonic Coanda Jet Nozzles
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Bevilaqua, P.M.1
Lee, J.D.2
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Including a BASIC Computer Program
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Garner, D., "No Moving Parts, The Circulation Control Airfoil and Fluidic Propeller, EAA Sport Aviation, Vol. No. 3, pp. 27-30, March, 1988.
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84894563265
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Pneumatic High-Lift and Control Surfaces Applied to Micro-Aerial Vehicles
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published in Conference, Atlanta, GA, February
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Englar, R. J., "Pneumatic High-Lift and Control Surfaces Applied to Micro-Aerial Vehicles," published in Conference Proceedings of GTRI International Conference on Emerging Technologies for Micro Air Vehicles, Atlanta, GA, February 19-20, 1997.
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Proceedings of GTRI International Conference On Emerging Technologies For Micro Air Vehicles
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West Virginia University, Dept of Aerospace Engr., Report TR-32, July
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Walters, R.E., et al., "Circulation Control by Steady and Pulsed Blowing for a Cambered Elliptic Airfoil," West Virginia University, Dept of Aerospace Engr., Report TR-32, July, 1972.
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Circulation Control By Steady and Pulsed Blowing For a Cambered Elliptic Airfoil
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Development of Pneumatic Aerodynamic Concepts for Control of Lift, Drag, Moments and Lateral/Directional Stability of Automotive Vehicles
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SAE Paper 960673, February 26-29, 1996; also published in SAE SP-1145, February
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Englar, Robert J., M. J. Smith, C. S. Niebur and S. D. Gregory, "Development of Pneumatic Aerodynamic Concepts for Control of Lift, Drag, Moments and Lateral/Directional Stability of Automotive Vehicles," SAE Paper 960673, February 26-29, 1996; also published in SAE SP-1145, "Vehicle Aerodynamics", February, 1996.
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(1996)
Vehicle Aerodynamics
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Englar, R.J.1
Smith, M.J.2
Niebur, C.S.3
Gregory, S.D.4
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64
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Development of Pneumatic Aerodynamic Devices to Improve the Performance
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Englar R. J., "Development of Pneumatic Aerodynamic Devices to Improve the Performance, Economics, and Safety of Heavy Vehicles," SAE Paper 2000-01-2208, June, 2000.
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Economics, and Safety of Heavy Vehicles
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Englar, R.J.1
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