Introduction
Concept
Mission
Principles
Blowing System
Short Field
Comfort-RideTM
Lift Control
Extended Glide
Feasibility
Specifications
References
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This document was printed from http://www.razak.com.
© 2003 Razak Engineering, Inc. All rights reserved.
- Nunemaker,J.J. and Fisher, J. W., "Two Dimensional Wind Tunnel Investigation of Boundary Layer Control by Blowing on an NACA 23015 Airfoil," ONR Engineering Report No. 203, April 1950.
- Stalter, J.L., "Circulation Control Research - Wind Tunnel Tests of a Powered, Blowing-Type, Circulation Control Research Airplane Model, "ONR Engineering Reports No. 187-1 through 187-6, December 1956 through February 1958.
- Stalter, J.L. and Wattson Jr., R. K., "Experimental Investigation of a Means of Obtaining Independent Control of Lift and Drag in Landing Approach," UWER No. 315-5. The University of Wichita, 1959 (Performed Under contract DA 44-177-TC-356 for United States Army Transportation Research and Engineering Command, Fort Eustis, VA).
- Nicolai, L.M., "Fundamentals of Aircraft Design", Nicolai, San Jose, CA, Distributed by METS, 1984.
- Stickle, Joseph W., Patton, James M., Henry, Robert C., "Flight Tests of a Direct Lift Control System During Approach and Landing". NASA TN D-4854. Langley Research Center, Langley Station, Hampton, VA. June 10, 1968.
- Chilton, Robert G., "Some Measurements of Atmospheric Turbulence Obtained From Flow-Direction Vanes Mounted On An Airplane," NACA, Technical Note 3313, Langley Aeronautical Laboratory, Langley Field, VA. November 1954.
- Kraft, Jr., Christopher C., "Initial Results Of A Flight Investigation Of A Gust-Alleviation System," NACA, Technical Note 3612, Langley Field, VA., Langley Field, VA. April 1956.
- Razak, Kenneth, "Summary Report, The Distributor Wing Agricultural Airplane". Razak Engineering, Inc. September 1997.
- Nagati, M. Gawad, Rokhsaz, Kamran, "Conceptual Design Of A Propulsion Wing Aircraft". Wichita State University, Wichita, Kansas January 30, 2000.
This document was printed from http://www.razak.com.
© 2003 Razak Engineering, Inc. All rights reserved.
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