This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Distributed Suction Boundary Layer Control for High Lift
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1968 by SAE International in United States
Annotation ability available
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.
CitationRoberts, S., "Distributed Suction Boundary Layer Control for High Lift," SAE Technical Paper 680645, 1968, https://doi.org/10.4271/680645.
- Tani, I. “Critical Survey of Published Theories on the Mechanism of Leading-Edge Stall.” University of Tokyo Report No. 367 1961
- Ludwieg H. Tillmann, W. “Investigation of the Wall Shearing Stress in the Turbulent Boundary Layer.” NACA TM 1285 1949
- Roberts, S. C. Smith, M. R. Clark, D. G. “Flight Test Evaluation of a Distributed Suction High-Lift Boundary Layer Control System on a Modified L-19 Liaison Aircraft.” USAAVLABS Tech. Report 66–36 1966
- 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 Unpublished Report, Department of Aerophysics and Aerospace Engineering, Mississippi State University
- Pechau, W. “Calculation of the Turbulent Boundary Layer with Continuously Distributed Suction.” AGARD Report No. 259 1960
- Mertaugh, L. “XV-11A Detail Specifications.” Department of Aerophysics and Aerospace Engineering, Mississippi State University 1967
- Clark, D. G. “Flight Development of a High-Lift Research Aircraft Using Distributed Suction.” Presented at the AGARD Flight Mechanics Panel Paris 1965
- Weiburg J. A. Gamse, B. “Large Scale Wind Tunnel Tests of an Airplane Model with Two Propellers and Rotating Cylinder Flaps.” NACA TND-4489 March 1968
- Davidson J. D. Ferry, R. G. “TL-19D Phase IV Performance.” AD No. 124109 1957