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Distributed Suction Boundary Layer Control for High Lift
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English
Abstract
The evolution of a successful distributed suction boundary layer control system is described, and an analysis of various high-lift aircraft has been performed to determine the wing lift and the increment of lift due to boundary layer control. Operational problems of distributed suction boundary layer control aircraft are discussed, and a comparison with other means of achieving similar lift coefficients is made.
Authors
Citation
Roberts, S., "Distributed Suction Boundary Layer Control for High Lift," SAE Technical Paper 680645, 1968, https://doi.org/10.4271/680645.Also In
References
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- Cornish J. J. III “Some Aerodynamic and Operational Problems of STOL Aircraft With Boundary Layer Control.” Presented at the AIAA Conference Wichita 1964
- Roberts S. C. Burt, S. “Analysis of the Turbulent Boundary Layer on the Distributed Suction High-Lift Wing of an L-19 Aircraft.” Unpublished Report, Department of Aerophysics and Aerospace Engineering, Mississippi State University
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